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Bovine leukosis -- Transmission

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• Bovine leukosis
• Transmission

• Bovine leukosis : transmission (Ohio Agricultural Research and Development Center, 1972), by R. F. Cross (page images at HathiTrust; US access only)

Items below (if any) are from related and broader terms.

• Studies of leukosis enzootica bovis, with special regard to diagnosis, epidemiology, and eradication. (U.S. National Cancer Institute; for sale by the Supt. of Docs., U.S. Govt. Print. Off., 1966), by Hans Jørgen Bendixen (page images at HathiTrust; US access only)
• Proceedings of Bovine Leukosis Symposium, May 22-23, 1979, University of Maryland, College Park, Maryland (s.n.], 1979), by College Park Bovine Leukosis Symposium, United States. Science and Education Administration, and United States. Animal and Plant Health Inspection Service. Veterinary Services (page images at HathiTrust; US access only)

• Proceedings of Bovine Leukosis Symposium, May 22-23, 1979, University of Maryland, College Park, Maryland (s.n.], 1979), by College Park Bovine Leukosis Symposium, United States. Science and Education Administration, and United States. Animal and Plant Health Inspection Service. Veterinary Services (page images at HathiTrust; US access only)

• Transmission of power; the present, the future (E.& F.N. Spon, Ltd., 1926), by George Constantinesco (page images at HathiTrust; US access only)
• Die transmission Justinian's insbesondere das wissen oder nichtwissen des transmittirenden erben. (Leipzig, 1859), by Karl Wieding (page images at HathiTrust)

• Delation der Erbschaft im falle einer todtgeburt. (München, 1876), by Georgius Altenrath (page images at HathiTrust)

• Do Insects Transmit AIDS? (Washington: Office of Technology Assessment, 1987), by Lawrence H. Miike and United States Congress Office of Technology Assessment
  • page images at HathiTrust
  • PDF files at Princeton
• Social Networks, Drug Abuse, and HIV Transmission, ed. by Richard Needle, Susan L. Coyle, Sander G. Genser, and Robert T. Trotter (PDF at NIH)
• Social networks, drug abuse, and HIV transmission (U.S. Dept. of Health and Human Services, Public Health Service, National Institutes of Health, National Institute on Drug Abuse, 1995), by Richard Needle and National Institute on Drug Abuse (page images at HathiTrust)

• Brookhaven lecture series : radioastronomy and communication through space (Brookhaven National Laboratory, 1960), by Edward M. Purcell, Brookhaven National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)

• Preliminary experiments in the transmission of anaplasmosis by horseflies (Oklahoma Agricultural and Mechanical College, Agricultural Experiment Station, 1932), by C. E. Sanborn, George Whitfield Stiles, and Lewis H. Moe (page images at HathiTrust; US access only)
• The Transmission of anaplasmosis by horseflies (Tabanidae) (Oklahoma Agricultural and Mechanical College, Agricultural Experiment Station, 1941), by D. E. Howell (page images at HathiTrust; US access only)

• The Effects on Human Health of Subtherapeutic Use of Antimicrobials in Animal Feeds (1980), by Assembly of Life Sciences (U.S.) (page images at NAP)

• The effects of resonant acoustic vibrations on the local and overall heat transfer coefficients for air flowing though an isothermal horizontal tube (Wright-Patterson Air Force Base, Ohio : Aeronautical Research Laboratory, Air Force Research Division, Air Research and Development Command, United States Air Force, 1960., 1960), by Thomas Woodrow Jackson, Harold L. Johnson, Calvin C. Oliver, Kenneth R. Purdy, Aerospace Research Laboratories (U.S.), and Georgia Institute of Technology (page images at HathiTrust)
• Experimental heat transfer to blunt axisymmetric bodies near the limit of continuum flow (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1962., 1962), by J. Leith Potter, John T. Miller, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)

• SARS: Down But Still a Threat (National Intelligence Council ICA 2003-09, 2003), by Karen Monaghan (page images at HathiTrust)
• Notes on the relation of insects to disease. Lecture outlines of course 23 in entomology. (Ithaca Journal, 1912), by William A. Riley (page images at HathiTrust)
• Epidemiology and control of vector-borne diseases (U.S. Dept of Health, Education, and Welfare, Public Health Service, Communicable Disease Center, 1963), by Harry D. Pratt (page images at HathiTrust)
• Prevention and control of vector problems. (Fort Collins, Colo., 1975), by Center for Disease Control. Vector-Borne Diseases Division. Water Resources Branch (page images at HathiTrust)
• Protection of domesticated animals. ([n.p.], 1913), by Veranus A. Moore (page images at HathiTrust; US access only)
• The cat in relation to disease transmission: a review. (Cold Spring Harbor, N. Y., 1931), by Denis R. A. Wharton (page images at HathiTrust)
• Effect of poultry diseases on the egg. (Ithaca, 1945), by Theodore Dubin (page images at HathiTrust)
• A report on the influence of milk in spreading zymotic disease, with a tabular analysis of 48 outbreaks. (Smith, Elder & Co., 1897), by Ernest Hart (page images at HathiTrust)
• Diseases of animals communicable to man. ([n.p., 1927), by Veranus A. Moore (page images at HathiTrust)
• Proceedings. (U. S. Govt. Print. Off., 1956), by Regional meetings on foreign animal diseases. 1956 and United States. Agricultural Research Service (page images at HathiTrust)
• A treatise on the means of purifying infected air, of preventing contagion, and arresting its progress (Printed by J.& E. Hodson for T. Hurst, 1802), by Louis-Bernard Guyton de Morveau (page images at HathiTrust)
• Infection control manual : a policy and procedure manual. ([Dept. of Defense, Dept. of the Army], Walter Reed Army Medical Center, 1977), by Walter Reed Army Medical Center (page images at HathiTrust; US access only)
• The carrier problem in infectious diseases (E. Arnold ;, 1912), by J. C. G. Ledingham and J. A. Arkwright (page images at HathiTrust; US access only)
• Restriction and prevention of the dangerous communicable diseases (s.n., 1890), by A. Arnold Clark (page images at HathiTrust; US access only)
• The role of ptomaines in infectious diseases. (Providence Press, 1889), by Charles V. Chapin (page images at HathiTrust)
• Zygomycosis caused by Apophysomyces elegans (U.S. Dept. of Health and Human Services, Public Health Service, 1985), by Marion A. Wieden and United States Public Health Service (page images at HathiTrust)
• Experiments to determine if paralyzed domestic animals and those associated with cases of infantile paralysis may transmit this disease. (Wright & Potter, 1914), by Carl Ten Broeck (page images at HathiTrust)
• Indicators of viruses in water and food (Ann Arbor Science, 1978), by United States Environmental Protection Agency (page images at HathiTrust)
• Waterborne disease outbreaks : selected reprints of articles on epidemiology, surveillance, investigation, and laboratory analysis (Health Effects Research Laboratory, Office of Research and Development, U.S. Environmental Protection Agency, 1990), by Gunther F Craun and Ohio) Health Effects Research Laboratory (Cincinnati (page images at HathiTrust)
• Guidelines for analysis of communicable disease control planning (U.S. Dept. of Health, Education, and Welfare, Public Health Service, Office of the Assistant Secretary for Health, Office of International Health, 1979), by Florence R Morrison, James Chin, United States. Agency for International Development. Office of Health, E.H. White Company, and United States. Office of International Health (page images at HathiTrust; US access only)
• Arthropods of medical importance in Africa (Natick, Mass., 1967), by B. V. Travis, Celso E. Mendoza, Renato M. Labadan, United States. Office of the Quartermaster General, and Cornell University. College of Agriculture (page images at HathiTrust)

• Electromagnetic surface fields due to a magnetic dipole buried in a three-layered earth (U.S. Dept. of the Interior, Bureau of Mines, 1982), by S. M. Shope and United States Bureau of Mines (page images at HathiTrust)
• Test of butterfly valve with magnetic transmission (Atomic Energy Commission, 1944), by Stanford Neal and U.S. Atomic Energy Commission Technical Information Branch (page images at HathiTrust)
• Effect of ultralow frequency signaling on blasting array current (U.S. Dept. of the Interior, Bureau of Mines, 1993), by Kenneth E. Hjelmstad, Russell E. Griffin, and United States Bureau of Mines (page images at HathiTrust)
• A probabilistic model for predicting the duration of levels of electromagnetic transmission in falling snow (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1984., 1984), by Rosemary M. Dyer and U.S. Air Force Geophysics Laboratory. Atmospheric Sciences Division (page images at HathiTrust)
• The Transmission of electromagnetic waves in the presence of a conducting layer of gas ([Washington, D.C.] : [United States Air Force, Office of Scientific Research], 1959., 1959), by G. S. S. Ludford, United States. Air Force. Office of Scientific Research, and College Park. Institute for Fluid Dynamics and Applied Mathematics University of Maryland (page images at HathiTrust)

• Epidemiologic studies of virus transmission in swimming waters (Health Effects Research Laboratory, Office of Research and Development, U.S. Environmental Protection Agency ;, 1980), by Donn J. D'Alessio, University of Wisconsin--Madison, Ohio). Field Studies Division Health Effects Research Laboratory (Cincinnati, and Ohio) Health Effects Research Laboratory (Cincinnati (page images at HathiTrust)

• Insect transmission of swamp fever or infectious anemia of horses (University of Wyoming, Agricultural Experiment Station, 1922), by John W. Scott and Wyoming Agricultural Experiment Station (page images at HathiTrust)
• The experimental transmission of swamp fever or infectious anemia by means of secretion (University of Wyoming, Agricultural Experiment Station, 1924), by John W. Scott and Wyoming Agricultural Experiment Station (page images at HathiTrust)

• Analysis of neutron transmission through slabs of lithium hydride (Atomics International, 1965), by R. S. Hubner, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)

• The metamorphosis of Filaria sanguinis hominis in the mosquito (s.n.], 1884), by Patrick Manson and Linnean Society of London (page images at HathiTrust)

• Ballistic Range Measurements of Stagnation-Point Heat Transfer in Air and Carbon Dioxide at Velocities up to 18,000 Feet per Second (NASA technical note D-777; Washington: National Aeronautics and Space Administration, 1961), by Layton Yee, Harry E. Bailey, and Henry T. Woodward (page images at HathiTrust)
• Heat Transfer (first edition; New York et al.: McGraw-Hill, 1961), by Benjamin Gebhart (page images at HathiTrust)
• Fluid Dynamics and Heat Transfer (New York: McGraw-Hill, 1958), by James George Knudsen and Donald L. Katz (page images at HathiTrust)
• A Heat Transfer Textbook (electronic edition), by John H. Lienhard (PDF at MIT; geographic and occupation information required)
• Engineering Data on Flow of Fluids in Pipes and Heat Transmission (Chicago: Crane Co., c1935), by Crane Co. Engineering Division (page images at HathiTrust)
• Heat transfer lectures : [given at the NEPA heat transfer symposium, December 8-13, 1947] (Oak Ridge, 1948), by Fairchild Hiller Corporation. Nuclear Energy Power for Aircraft Division and Don Cowen (page images at HathiTrust)
• Heat transfer and evaporation (The Chemical catalog company, inc., 1926), by Walter L. Badger (page images at HathiTrust)
• Handbook of heat transfer media. (Reinhold, 1962), by Paul L. Geiringer (page images at HathiTrust)
• Thermodynamics, fluid flow and heat transmission (McGraw-Hill book company, inc., 1938), by Huber O. Croft (page images at HathiTrust; US access only)
• Heat transfer. (Wiley, 1949), by Max Jakob (page images at HathiTrust)
• Principles of heat transfer. (International Textbook Co., 1958), by Frank Kreith (page images at HathiTrust)
• The influence of small concentrations of air in steam on the steam-film coefficient of heat transfer. ([Philadelphia, 1935), by Stanley John Meisenburg, Walter L. Badger, and Robert Marsh Boarts (page images at HathiTrust)
• Die Grundlagen der Wärmeübertragung (T. Steinkopff, 1927), by Friedrich Merkel (page images at HathiTrust; US access only)
• Heat transfer notes for electrical engineering. (G. Wahr, 1938), by A. D. Moore (page images at HathiTrust)
• Advanced heat transfer. (published in cooperation with Engineering Publications Office, College of Engineering; University of Illinois Press, 1969), by University of Illinois Advanced Heat Transfer Short Course, Pʻei-chih Chao, American Society of Mechanical Engineers, and University of Illinois at Urbana-Champaign (page images at HathiTrust)
• Die wärmeübertragung; ein lehr- und nachshlagebuch für den praktischen gebrauch (J. Springer, 1927), by M. ten Bosch (page images at HathiTrust; US access only)
• Numerical analysis of heat flow. (McGraw-Hill, 1949), by George Merrick Dusinberre (page images at HathiTrust)
• The calculation of heat transmission (H.M. Stationery Off, 1932), by M. Fishenden and Owen Albert Saunders (page images at HathiTrust)
• Einführung in die lehre von der wärmeübertragung (J. Springer, 1926), by Heinrich Gröber (page images at HathiTrust; US access only)
• Recent advances in heat and mass transfer. (McGraw-Hill, 1961), by J. P. Harnett (page images at HathiTrust)
• Industrial heat transfer (Industrial Press, 1952), by Francis William Hutchinson (page images at HathiTrust)
• Flow of fluids through valves, fittings and pipe (Crane co., 1942), by Crane (Firm) (page images at HathiTrust)
• Principles of engineering heat transfer. (Van Nostrand, 1957), by Warren H. Giedt (page images at HathiTrust)
• The simple and direct answer to all problems of heat transfer in boilers (s.n., 1937), by Loyd Richard Stowe (page images at HathiTrust)
• Heat transfer in miniaturized electronic equipment. (Bureau of Ships, Navy Dept., 1955), by Cornell Aeronautical Laboratory (page images at HathiTrust)
• Heating asphalt with diphenyl vapor ([Ann Arbor, Mich.] : [publisher not identified], 1932., 1932), by Warren L. McCabe (page images at HathiTrust)
• Performance of louvered devices as air mixers (U.S. National Bureau of Standards; for sale by the Supt. of Docs., U.S. Govt. Print. Off, 1970), by T. K. Faison, Paul R. Achenbach, and Joseph C. Davis (page images at HathiTrust)
• The Rayleigh problem for a dissociated gas ([Buffalo, N.Y.], 1961), by F. K. Moore, W.J. Rae, and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Heat transfer notes for electrical engineering (G. Wahr, 1942), by A. D. Moore (page images at HathiTrust)
• Heat transfer notes (University of California Press, 1946), by Llewellyn Michael Kraus Boelter, Raymond Constantine Martinelli, Harold Alexander Johnson, and V. H. Cherry (page images at HathiTrust)
• Die Grundgesetze der Wärmeleitung und des Wärmeüberganges : ein Lehrbuch für Praxis und technische Forschung (J. Springer, 1921), by Heinrich Gröber (page images at HathiTrust; US access only)
• Standards of tubular exchanger manufacturers association ... (Tubular exchanger manufacturers association, inc., 1941), by inc. Tubular exchanger manufacturers association (page images at HathiTrust)
• Heated surface jet discharged into a flowing ambient stream (U.S. Environmental Protection Agency; [for sale by the Supt. of Docs., U.S. Govt. Print. Off.], 1972), by Louis H Motz, Barry A Benedict, and United States Environmental Protection Agency (page images at HathiTrust)
• Performance of square-edged orifices and orifice-target combinations as air mixers (U.S. National Bureau of Standards; for sale by the Supt. of Docs., U.S. Govt. Print. Off, 1967), by T K. Faison, Paul R. Achenbach, and Joseph C. Davis (page images at HathiTrust)
• Boiling heat transfer for oxygen, nitrogen, hydrogen, and helium (U.S. National Bureau of Standards :, 1965), by E. G. Brentari, R. V. Smith, P. J. Giarratano, and United States. National Bureau of Standards (page images at HathiTrust)
• Der Wärmeübergang und die thermodynamische Berechnung der Leistung bei Verpuffungsmaschinen insbesondere bei Kraftfahrzeug-Motoren (Verlag von Julius Springer, 1925), by August Herzfeld (page images at HathiTrust; US access only)
• LMFBR fuel analysis : task B : post-accident heat removal : final report, October 1, 1976-September 30, 1977 / c J. Castle ... [et al.]. (Nuclear Regulatory Commission, Office of Nuclear Reactor Regulation, Division of Project Management ;, 1978), by J. Castle and U.S. Nuclear Regulatory Commission. Division of Project Management (page images at HathiTrust)
• Bubble behavior in LMFBR core disruptive accidents : annual report October, 1977-September, 1978 (The Commission ;, 1979), by C. A. Erdman, University of Virginia. Department of Nuclear Engineering and Engineering Physics, and U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research (page images at HathiTrust)
• Heat transfer and carryover of low pressure water in a heated vertical tube (Massachusetts Institute of Technology ;, 1976), by Thomas Alfred Smith and U.S. Nuclear Regulatory Commission (page images at HathiTrust)
• Bubble behavior in LMFBR core disruptive accidents : annual report, July 1, 1976 - September 30, 1977 (Division of Reactor Safety Research, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commision ;, 1978), by Albert B. Reynolds, C. A. Erdman, U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research, and University of Virginia. Department of Nuclear Engineering (page images at HathiTrust)
• Bubble behavior in LMFBR core disruptive accidents : annual report, October 1979 - September 1980 (Division of Accident Evaluation, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission :, 1981), by Albert B. Reynolds, U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Accident Evaluation, and University of Virginia. Department of Nuclear Engineering and Engineering Physics (page images at HathiTrust)
• Improved reliability of residual heat removal capability in PWRs as related to resolution of Generic issue 99 (Division of Reactor and Plant Systems, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1988), by T. L. Chu, Brookhaven National Laboratory, and U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Reactor and Plant Systems (page images at HathiTrust)
• Natural convection heat transfer in beds of inductively heated particles (U.S. Nuclear Regulatory Commission, Office of Nuclear Regulatory Research, Division of Reactor Safety Research ;, 1978), by Seung Joon Rhee, V. K. Dhir, and U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research (page images at HathiTrust)
• Study of thermal and hydrodynamic processes associated with melting of horizontal substrate (Nuclear Regulatory Commission, Office of Nuclear Regulatory Research, Division of Reactor Safety Research, 1979), by Kaveh Taghavi-Tafreshi, V. K. Dhir, Los Angeles. School of Engineering and Applied Science University of California, and U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research (page images at HathiTrust)
• LMFBR fuel analysis task B : post-accident heat removal : final report, October 1977 - November 1978 (Division of Project Management, Office of Nuclear Reactor Regulation, U.S. Nuclear Regulatory Commission ;, 1979), by I. Catton, U.S. Nuclear Regulatory Commission. Division of Project Management, and Los Angeles. School of Engineering and Applied Science University of California (page images at HathiTrust)
• A phenomenological correlation for post-CHF heat transfer (Nuclear Regulatory Commission, 1977), by John C. Chen, F. T. Ozkaynak, R. K. Sundaram, and U.S. Nuclear Regulatory Commission (page images at HathiTrust)
• Study of dryout heat fluxes in beds of inductively heated particles (Division of Reactor Safety Research, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission ;, 1977), by V. K. Dhir, W. E. Kastenberg, I. Catton, U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research, and Los Angeles. School of Engineering and Applied Science University of California (page images at HathiTrust)
• Transient natural convection in an internally heated fluid layer : topical report, June 1975 - June 1976 (U.S. Nuclear Regulatory Commission ;, 1976), by F. A. Kulacki, A. A. Emara, U.S. Nuclear Regulatory Commission, and Ohio State University. Department of Mechanical Engineering (page images at HathiTrust)
• Theoretical investigations of the transition from bubble boiling to film boiling at forced convection. (U.S. Nuclear Regulatory Commission, 1978), by O. Kampfenkel, U.S. Nuclear Regulatory Commission, Kraftwerk Union Aktiengesellschaft. Hauptbereich Reaktortechnik, and Germany. Bundesministerium für Forschung und Technologie (page images at HathiTrust)
• Steady and transient natural convection with volumetric energy sources in a fluid layer bounded from below by a segment of a sphere : annual report, July 1976 - September 1977 (The Commission, 1978), by J. H. Min, F. A. Kulacki, and U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research (page images at HathiTrust)
• Condensation rates in steam-water mixing : quarterly progress report, June 1, 1977 - September 1, 1977 (Division of Reactor Safety Research, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission ;, 1978), by S. G. Bankoff, M. C. Yuen, R. S. Tankin, U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research, and Ill.) Northwestern University (Evanston (page images at HathiTrust)
• Marangoni convection in a gravity-free silicon float zone (Carderock Division, Naval Surface Warfare Center, 1994), by Samuel Ohring, Hans J. Lugt, and Naval Surface Warfare Center (U.S.). Carderock Division (page images at HathiTrust)
• Problems of heat transfer (U.S. Atomic Energy Commission, Division of Technical Information, 1961), by M. A. Mikheev and U.S. Atomic Energy Commission. Division of Technical Information (page images at HathiTrust; US access only)
• Heat transfer to liquid metals in concentric annuli (Oak Ridge National Laboratory, 1950), by Raymond V. Bailey (page images at HathiTrust)
• Heat transfer, burnout, and pressure drop for water in swirl flow through tubes with internal twisted tapes (Oak Ridge National Laboratory, 1960), by W. R. Gambill (page images at HathiTrust)
• Snow and ice removal from pavements using stored earth energy. Final report. (1974), by Walter B. Bienert, M. F. Pravda, H. J. Suelau, and D. A. Wolf (page images at HathiTrust)
• Prevention of preferential bridge icing using heat pipes. Interim report. (1975), by Angelo A. Ferrara and R. Haslett (page images at HathiTrust)
• Temperature effects on rolling resistance of pneumatic tires. Interim report. (1976), by Samuel K. Clark and M. Loo (page images at HathiTrust)
• Higher strength steels specially processed for high heat input welding. (1985) (page images at HathiTrust; US access only)
• Die Wärmeverluste durch ebene Wände unter besonderer Berücksichtigung des Bauwesens (R. Oldenbourg, 1921), by Karl Hencky (page images at HathiTrust; US access only)
• Feasibility, research and analysis of heat exchange systems without metallic heat exchange surfaces and laboratory study of single state vapor reheat distillation (U.S. Dept. of the Interior :, 1962), by David A. Oliver, E. D. Baird, William A. Shrode, Teynham Woodward, W. S. Thompson, United States. Office of Saline Water, and FMC Corporation. Central Engineering Laboratories (page images at HathiTrust)
• Experimental and analytical studies of heat transfer in a falling film system (U.S. Dept. of the Interior, [Office of Saline Water], 1967), by A. E. Dukler, L. C. Elliott, Inc Houston Research Institute, and United States. Office of Saline Water (page images at HathiTrust)
• Heat and mass transfer to particles suspended in agitated liquids (U.S. Dept. of the Interior, 1968), by Thomas K. Sherwood, P. L. T. Brian, Massachusetts Institute of Technology, and United States. Office of Saline Water (page images at HathiTrust)
• Lecture notes on heat extraction from boiling water power reactors (Argonne National Laboratory, 1959), by Paul A. Lottes, J. F. Marchaterre, Michael Petrick, Argonne National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Effect of a transverse magnetic field on vertical two-phase flow through a rectangular channel (Argonne National Laboratory, 1964), by Richard J. Thome, Argonne National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• An investigation of certain thermodynamic and transport properties of water and water vapor in the critical region (Argonne National Laboratory, 1959), by E. S. Nowak, R. J. Grosh, and Argonne National Laboratory (page images at HathiTrust)
• Performance characteristics of EBWR from 0 to 100 Mwt (Argonne National Laboratory, 1963), by H. Iskenderian, W. C. Lipinski, Michael Petrick, E. A. Wimmunc, Argonne National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• An empirical modification of nucleation theory and its application to boiling heat transfer (Argonne National Laboratory, 1961), by Yan-Po Chang, U.S. Atomic Energy Commission, and Argonne National Laboratory (page images at HathiTrust)
• A study of unsteady magnetohydrodynamic flow and heat transfer (Argonne National Laboratory, 1964), by Ralph M. Singer, U.S. Atomic Energy Commission, and Argonne National Laboratory. Reactor Engineering Division (page images at HathiTrust)
• Electrical end losses in an magnetohydrodynamic channel of linearly variable cross section (Argonne National Laboratory, 1965), by Jerzy R. Moszynski, U.S. Atomic Energy Commission, Argonne National Laboratory. Reactor Engineering Division, and Associated Midwest Universities (page images at HathiTrust)
• Channel-wall limitations in the magnetohydrodynamic induction generator (Argonne National Laboratory, 1966), by E. S. Pierson, William D. Jackson, U.S. Atomic Energy Commission, and Argonne National Laboratory. Reactor Engineering Division (page images at HathiTrust)
• An analytical investigation of laminar film boiling. (Argonne National Laboratory, 1959), by P. W. McFadden, R. J. Grosh, Purdue Research Foundation. Department of Mechanical Engineering, U.S. Atomic Energy Comission, and Argonne National Laboratory (page images at HathiTrust)
• Heat transfer with laminar flow in concentric annuli with constant and arbitrary variable axial wall temperature (Argonne National Laboratory, 1961), by R. Viskanta, U.S. Atomic Energy Comission, and Argonne National Laboratory. Reactor Engineering Division (page images at HathiTrust)
• Observations on transition boiling heat transfer phenomena (Argonne National Laboratory, Reactor Engineering Division, 1960), by Bernard J. Stock, U.S. Atomic Energy Commission, and Argonne National Laboratory. Reactor Engineering Division (page images at HathiTrust)
• An experimental investigation of high-flux free convection heat transfer to water up to near-critical conditions (Argonne National Laboratory, 1961), by Vernon Emerson Holt, U.S. Atomic Energy Commission, and Argonne National Laboratory (page images at HathiTrust; US access only)
• Boiling water reactor technology status of the art report. Volume II, Water chemistry and corrosion (Argonne National Laboratory, 1963), by C. R. Breden, U.S. Atomic Energy Comission, and Argonne National Laboratory. Reactor Engineering Division (page images at HathiTrust)
• Mixing of a cold liquid jet with a boiling liquid stream (Argonne National Laboratory, 1960), by S. G. Bankoff, U.S. Atomic Energy Commission, Argonne National Laboratory, and Thompson Ramo Wooldridge Incorporated. Research Laboratory Ramo-Wooldridge (page images at HathiTrust)
• A description of thermal conductivity and dynamic viscosity of water in the critical region (Argonne National Laboratory, 1960), by C. A. Fritsch, R. J. Grosh, U.S. Atomic Energy Commission, Argonne National Laboratory, and Purdue Research Foundation. Department of Mechanical Engineering (page images at HathiTrust)
• An experimental investigation of heat transfer to superheated steam in round and rectangular channels (Argonne National Laboratory, 1960), by J. B. Heineman, U.S. Atomic Energy Commission, and Argonne National Laboratory (page images at HathiTrust)
• Transfer of heat from helium at high temperatures : physical characteristics of ceramic heat exchangers (U.S. Dept. of the Interior, Bureau of Mines, 1962), by John J. S. Sebastian and Stanley C. Browning (page images at HathiTrust)
• The flow of coal-ash slag on furnace walls (U.S. Govt. print. off., Bureau of Mines, 1944), by P. Cohen and William Thomas Reid (page images at HathiTrust)
• A numerical method for determining heat-transfer characteristics for a dilute gas-solids mixture in an externally heated tube (U.S. Dept. of the Interior, Bureau of Mines, 1967), by Michael J. Lempel (page images at HathiTrust)
• Calculation procedure for heat transfer to a gas-solid suspension from an externally heated tube (United States Dept. of the Interior, Bureau of Mines, 1970), by M. B. Bransford, John H. Holden, and United States Bureau of Mines (page images at HathiTrust)
• Stability of a fin in boiling liquid (Atomic Energy Commission, 1947), by Gale Young and U.S. Atomic Energy Commission (page images at HathiTrust)
• Design and construction of a radiation probe (U.S. Dept. of Interior, Bureau of Mines, 1970), by C. H. Schwartz, A. A. Orning, and United States Bureau of Mines (page images at HathiTrust)
• Experiments with solid-in-gas suspensions as heat transport mediums (U.S. Dept. of the Interior, Bureau of Mines, 1963), by James P. McGee, D. E. Bluman, J. P. O'Leary, W. T. Abel, and United States Bureau of Mines (page images at HathiTrust)
• Problems in recovering thermal energy from molten salts (U.S. Dept. of the Interior, Bureau of Mines, 1961), by D. H. Baker, O. Q. Leone, R. L. Olson, R. A. Renner, and Thomas A. Henrie (page images at HathiTrust)
• Power required to circulate gas-solids suspensions (U.S. Dept. of the Interior, Bureau of Mines, 1967), by Charles N. Rosenecker, Harry G. Lucas, Neil H. Coates, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heat transfer coefficients for continuously recirculated gas-solid suspensions (U.S. Dept. of the Interior, Bureau of Mines, 1967), by C. N. Rosenecker, J. D. Spencer, N. H. Coates, A. F. Galli, and Dean E. Bluman (page images at HathiTrust)
• Numerical analysis of heat flow. (McGraw-Hill, 1949), by George Merrick Dusinberre (page images at HathiTrust)
• Numerical marching techniques for fluid flows with heat transfer (Scientific and Technical Information Office, National Aeronautics and Space Administration; [for sale by the Supt. of Docs., U.S. Govt. Print. Off.], 1973), by Robert W. Hornbeck (page images at HathiTrust)
• Die Wärmeübertragung; ein Lehrúnd Nachschlagebuch für den praktischen Gebrauch. (J. Springer, 1927), by Maurits ten Bosch (page images at HathiTrust; US access only)
• Heat transfer engineering. (Prentice-Hall, 1959), by Hilbert van Nydeck Schenck (page images at HathiTrust)
• Nȧgra utändska metoder för bestämning av värmeldningsförmȧgan hos byggnadsmaterial, av Ragnar Rison Schlyter. (Svenska teknologföreningens förlag, 1921), by Ragnar Ragnarson Schlyter (page images at HathiTrust; US access only)
• ʹEtude sur l'ʹevolution d'un probleme de physique; la propagation thermique dans les solides (J. Vrin, 1927), by Gaston Bachelard (page images at HathiTrust; US access only)
• Effect of soot on heat transmission in small boilers (U.S. Dept. of the Interior, Bureau of Mines, 1935), by P. Nicholls and C. E. Augustine (page images at HathiTrust)
• Thermal insulation (Infra Insulation Inc., 1950), by Alexander Schwartz and Inc Infra Insulation (page images at HathiTrust; US access only)
• Heat transfer in condensation and boiling (State Scientific and Technical Publishers of Literature on Machinery, 1952), by Samson Semenovich Kutateladze and United States. National Technical Information Service (page images at HathiTrust)
• Heat transfer at high rates to water with surface boiling (Massachusetts Institute of Technology, 1948), by W. H. McAdams, W. E. Kennel, J. N. Addoms, Argonne National Laboratory, and Massachusetts Institute of Technology. Department of Chemical Engineering (page images at HathiTrust)
• Heat transfer to superheated steam at high pressure ([Argonne National Laboratory], 1949), by W. H. McAdams, W. E. Kennel, J. N. Addoms, U.S. Atomic Energy Commission, Argonne National Laboratory, and Massachusetts Institute of Technology. Department of Chemical Engineering (page images at HathiTrust)
• The effect of pressure on boiling density in multiple rectangular channels (Argonne National Laboratory, 1956), by J. F. Marchaterre, U.S. Atomic Energy Commission, and Argonne National Laboratory. Reactor Engineering Division (page images at HathiTrust)
• The control of condensation heat transfer rates using an electromagnetic field (Argonne National Laboratory, 1964), by Ralph Mark Singer, U.S. Atomic Energy Commission, and Argonne National Laboratory. Reactor Engineering Division (page images at HathiTrust)
• Heat transfer and flow of helium in channels--practical limits for applications in superconductivity (U.S. Dept. of Commerce, National Bureau of Standards, 1976), by M. C. Jones, W. W. Johnson, United States. National Bureau of Standards, and Institute for Basic Standards (U.S.) (page images at HathiTrust)
• Thermal conductance at the interface of a solid and helium II (Kapitza conductance)* (U.S. National Bureau of Standards; for sale by the Supt. of Docs., U.S. Govt. Print. Off., 1969), by N. S. Snyder and United States. National Bureau of Standards (page images at HathiTrust)
• HFIR heat-transfer studies of turbulent water flow in thin rectangular channels (Oak Ridge National Laboratory, 1961), by W. R. Gambill, R. D. Bundy, U.S. Atomic Energy Commission, and Oak Ridge National Laboratory. Reactor Division (page images at HathiTrust)
• Heat transfer from spent reactor fuels during shipping : a proposed method for predicting temperature distribution in fuel bundles and comparison with experimental data (Oak Ridge National Laboratory, 1963), by J. S. Watson, U.S. Atomic Energy Commission, and Oak Ridge National Laboratory. Chemical Technology Division (page images at HathiTrust)
• Review of thermal conductivity and heat transfer in uranium dioxide (Oak Ridge National Laboratory, 1959), by V. J. Tennery and U.S. Atomic Energy Commission (page images at HathiTrust)
• Condensation of refrigerant vapors in a gravity-drained ice bed (U.S. Dept. of the Interior; for sale by the Supt. of Docs., U.S. Govt. Print. Off., 1971), by Kenneth A. Smith, Geoffrey Margolis, Adel F. Sarofim, and United States. Office of Saline Water (page images at HathiTrust)
• The construction of pulse-guide coaxial transmission lines (University of California Radiation Laboratory, 1956), by C. Norman Winningstad and Lawrence Radiation Laboratory (page images at HathiTrust)
• Fluid mechanics and heat transfer for gases (air, He, H₂ and N₂) flowing single phase in closed channels : bibliography (University of California Lawrence Radiation Laboratory, 1962), by Rose Kraft, Lawrence Radiation Laboratory, and Lawrence Livermore Laboratory (page images at HathiTrust)
• Rate of heat transmission from bare steam pipes underground (1917), by W. A. Warrick (page images at HathiTrust)
• A thermal comparison among several beverage can solar collectors (U.S. Dept. of Agriculture, Forest Service, North Central Forest Experiment Station, 1984), by Peter Y. S. Chen and Minn.) North Central Forest Experiment Station (Saint Paul (page images at HathiTrust)
• Analysis of the transient conduction of heat in long solid cylindrical fuel elements for nuclear reactors (Hanford Atomic Products Operation, 1956), by Frank Eugene Tippets, United States. Energy Research and Development Administration, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Report on heat transfer experiments concerning PRTR Mark I fuel elements (U.S. Atomic Energy Commission, 1960), by G. M. Hesson, United States. National Bureau of Standards, United States. Department of Energy. Office of Fusion Energy, United States. National Bureau of Standards. Fracture and Deformation Division, U.S. Atomic Energy Commission, United States. Energy Research and Development Administration, Hanford Works, and Hanford Atomic Products Operation. Reactor and Fuels Research and Development Operation (page images at HathiTrust)
• A study of heat transfer effects on aluminum corrosion. Part I (Hanford Atomic Products Operation, 1956), by D. R. de Halas, United States. Energy Research and Development Administration, U.S. Atomic Energy Commission, and Hanford Atomic Products Operation (page images at HathiTrust)
• Theory of heat and mass transfer in batch condensation of solids (Atomic Energy Commission, 1946), by W. I. Thompson and U.S. Atomic Energy Commission (page images at HathiTrust)
• Proceedings of 1963 high-temperature liquid-metal heat transfer technology meeting (Oak Ridge National Laboratory, 1963), by Oak Ridge National Laboratory and U.S. Atomic Energy Commission (page images at HathiTrust)
• Forced convection heat transfer in thermal entrance regions. Part I (Oak Ridge National Laboratory, 1951), by H. F. Poppendiek, U.S. Atomic Energy Commission, and Oak Ridge National Laboratory Reactor Technology Division (page images at HathiTrust)
• Forced convection heat transfer in thermal entrance regions. Part II (Oak Ridge National Laboratory, 1952), by H. F. Poppendiek, L. D. Palmer, U.S. Atomic Energy Commission, and Oak Ridge National Laboratory Reactor Experimental Engineering Division (page images at HathiTrust)
• A transient heat transfer analysis of the MTR mock-up (Oak Ridge National Laboratory, 1951), by H. F. Poppendiek, H. C. Claiborne, U.S. Atomic Energy Commission, and Oak Ridge National Laboratory Reactor Technology Division (page images at HathiTrust)
• Heat transfer in noncircular ducts : Part I (Oak Ridge National Laboratory, 1951), by H. C. Clairborne, U.S. Atomic Energy Commission, and Oak Ridge National Laboratory (page images at HathiTrust)
• Turbulent forced convection heat transfer in circular tubes containing molten sodium hydroxide (Oak Ridge National Laboratory, 1952), by H. W. Hoffman, U.S. Atomic Energy Commission, and Oak Ridge National Laboratory Reactor Experimental Engineering Division (page images at HathiTrust)
• Aluminum chloride as a thermodynamic working fluid and heat transfer medium (Oak Ridge National Laboratory, 1959), by R. F. Newton, A. P. Fraas, L. G. Epel, M. Blander, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Fused salt heat transfer. Part III, Forced-convection heat transfer in circular tubes containing the salt mixture NaNO₂-NaNO₃-KNO₃ (Oak Ridge National Laboratory, 1960), by H. W. Hoffman, S. I. Cohen, U.S. Atomic Energy Commission, Union Carbide Corporation, and Oak Ridge National Laboratory. Reactor Experimental Engineering Division (page images at HathiTrust)
• The effects of resonant vibrations on heat transfer at high reynolds numbers final report (Engineering Experiment Station, Georgia Institute of Technology, 1961), by Thomas Woodrow Jackson, Ian Eastwood, Calvin C. Oliver, Georgia Institute of Technology. Engineering Experiment Station, and University of California. Lawrence Radiation Laboratory (page images at HathiTrust; US access only)
• Die Grundlagen der Wärmeübertragung (Edwards Brothers, 1944), by Friedrich Merkel (page images at HathiTrust; US access only)
• Interim report on transient heat-transfer measurements of catalytic recombination in a step-function flow of atomic oxygen. (Cornell Aeronautical Laboratory, inc., 1962), by A. L. Myerson (page images at HathiTrust)
• Turbulent forced convection heat transfer in circular tubes containing sodium hydroxide. (Oak Ridge National Laboratory, 1952), by H. W. Hoffman (page images at HathiTrust)
• Interferometric measurement in a shock tube of dissociation rates for air and its component gases. (Ithaca, N. Y., 1959), by Stanley Richard Byron (page images at HathiTrust)
• Research on radiant energy transfer in an absorbing medium (Purdue University, School of Aeronautical and Engineering Sciences, 1961), by I. P. Kolchenogova and S. N. Shorin (page images at HathiTrust; US access only)
• Radiative transfer between surfaces of arbitrary spatial distribution of reflexion. (Purdue University, School of Aeronautical and Engineering Sciences, 1961), by G. L. Poli︠a︡k (page images at HathiTrust; US access only)
• Mechanisms for increasing the peak heat flux in boiling saturated water at atmospheric pressure; a report for National Science Foundation, Grant GP 788. (University of Washington [College of Engineering], 1963), by Ward J. Frea (page images at HathiTrust)
• A study of the critical heat flux in an accelerating pool boiling system (Dept. of Mechanical Engineering, University of Washington, 1962), by Jim M. Adams (page images at HathiTrust)
• Pre-development study of a heat flux measurement device suitable for use on flight vehicles (Buffalo, 1962), by Cornell Aeronautical Laboratory and F. A. Vassallo (page images at HathiTrust)
• Rate of heat-transfer near the stagnation point of a blunt body of revolution, in the presence of a magnetic field. (Physical Research Laboratory, Space Technology Laboratories, a Division of the Ramo-Woolridge Corp., 1958), by Rudolph X. Meyer (page images at HathiTrust)
• Improved measurements of surface heat transfer by the method of cyclic temperature variations (U. S. Atomic Energy Commission, Technical Information Service, 1952), by Russell Wendt Dayton (page images at HathiTrust)
• Heat transfer by combined conduction and radiation through a radiating gas. (Air Force Institute of Technology, Air University, U. S. Air Force, School of Engineering], 1964), by Carl Gene Stolberg (page images at HathiTrust)
• Heat transfer and thermodynamic modeling (Distributed by U.S. Dept. of Commerce, Office of Technical Services, 1962), by Ėnergeticheskiĭ institut im. G.M. Krzhizhanovskogo (page images at HathiTrust)
• An investigation of laminar heat transfer to slender cones in the hypersonic shock tunnel (Cornell Aeronautical Laboratory, 1961), by Charles E. Wittliff and Merle R. Wilson (page images at HathiTrust)
• Skin friction, heat transfer, and pressure measurements on hypersonic inlet compression surfaces in the Mach number range 7.5 to 16 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1965., 1965), by M. O. Ryder, Cornell Aeronautical Laboratory, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Industrial development of atomic energy (U.S. Atomic Energy Commission. Technical Information Branch, 1948), by H. Etherington, Oak Ridge National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Flow of heat into coating through a narrow strip (U.S. Atomic Energy Commission. Technical Information Division, 1944), by William Karush, G. Young, Clinton Laboratories, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Temperature rise in a pitted surface (U.S. Atomic Energy Commission. Technical Information Service, 1944), by William Karush, Clinton Laboratories, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Temperature rise under uncooled areas of thin plates (U.S. Atomic Energy Commission. Technical Information Division, 1945), by William Karush, Clinton Laboratories, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Temperature of two metals in contact (U.S. Atomic Energy Commission. Technical Information Service, 1944), by William Karush, United States. Office of Scientific Research and Development. Metallurgical Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heat flow from a fin to a boiling liquid (U.S. Atomic Energy Commission. Technical Information Service, 1945), by A. V. Martin, Clinton Laboratories, and U.S. Atomic Energy Commission (page images at HathiTrust)
• The influence of "tube" size on the shape of the reactor for a specified heat transfer and flow friction performance (U.S. Atomic Energy Commission. Technical Information Service, 1947), by A. L. London, Inc. Rand Project Douglas Aircraft Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heat-transfer and friction-flow characteristics of cylindrical parallel rods with transverse cylindrical spacers (U.S. Atomic Energy Commission. Technical Information Service, 1954), by R. E. Grimble, S. L. Fawcett, W. H. Bell, Battelle Memorial Institute, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heat transfer and fluid flow studies with boundary layer turbulence promoters (Aerojet-General Corporation, Aerojet-General Nucleonics, 1963), by Nicholas Kattchee, W. V. Mackewicz, and Aerojet-General Corporation Aerojet-General Nucleonics (page images at HathiTrust)
• HECTIC-II : an IBM 7090 FORTRAN computer program for heat transfer analysis of gas or liquid-cooled reactor passages (Aerojet-General Corporation, Aerojet-General Nucleonics, 1962), by Nicholas Kattchee, William C. Reynolds, and Aerojet-General Corporation Aerojet-General Nucleonics (page images at HathiTrust)
• Biphenyl liquid heat transfer and vapor deposition studies at 700° and 800° : final report, February 9, 1961 to May 31, 1963 (U.S. Atomic Energy Commission, Division of Technical Information, 1963), by C. D. Jr King, W. J. Moodie, Monsanto Research Corporation, and Dayton Laboratory (page images at HathiTrust)
• Organic coolant summary report (U.S. Atomic Energy Commission, Idaho Operations Office, 1964), by R. F. Makens, Quincey L. Baird, and U.S. Atomic Energy Commission Idaho Operations Office Nuclear Technology Division Reactor Technology Branch (page images at HathiTrust)
• Transient response of the Engineering test reactor primary water temperature controller (U.S. Atomic Energy Commission, Idaho Operations Office, 1958), by W. J. Byron, S. R. Gossmann, and Phillips Petroleum Company. Atomic Energy Division (page images at HathiTrust)
• Stability analysis of the engineering test reactor with reactivity feedback through the temperature coefficient (U.S. Atomic Energy Commission, Idaho Operations Office, 1958), by S. R. Gossmann and Phillips Petroleum Company. Atomic Energy Division (page images at HathiTrust)
• Heat transfer in the engineering test reactor (U.S. Atomic Energy Commission, Idaho Operations Office, 1958), by V. A. Walker, Phillips Petroleum Company. Atomic Energy Division, and U.S. Atomic Energy Commission. Idaho Operations Office (page images at HathiTrust)
• Calculated surface temperatures for nuclear systems and analysis of their uncertainties : the first report of the Heat Transfer Subcommittee of the Phillips Reactor Safeguard Committee (U.S. Atomic Energy Commission, Idaho Operations Office, 1957), by R. J. Nertney and Phillips Petroleum Company. Atomic Energy Division (page images at HathiTrust)
• A four-region, two-group calculation of SPERT III critical size and flux distribution (U.S. Atomic Energy Commission, Idaho Operations Office, 1957), by Dale Robert Metcalf, V. C. Kobold, and Phillips Petroleum Company. Atomic Energy Division (page images at HathiTrust)
• Heat transfer in engineering test reactors fuel assemblies for cycle 13 (U.S. Atomic Energy Commission, Idaho Operations Office, 1959), by V. A. Walker and Phillips Petroleum Company. Atomic Energy Division (page images at HathiTrust)
• Materials Testing Reactor gamma heat generation measurements (U.S. Atomic Energy Commission, Idaho Operations Office, 1961), by L. D. Weber, Calvin H. Hogg, Phillips Petroleum Company. Atomic Energy Division, and Idaho National Reactor Testing Station (page images at HathiTrust)
• Engineering Testing Reactor gamma heat generation measurements for cycles 27, 33, and 34 (U.S. Atomic Energy Commission, Idaho Operations Office, 1961), by L. D. Weber, Calvin H. Hogg, Phillips Petroleum Company. Atomic Energy Division, and Idaho National Reactor Testing Station (page images at HathiTrust)
• Structural and heat-transfer properties of "U.S.S. Panelbilt" prefabricated sheet-steel constructions for walls, partitions, and roofs sponsored by the Tennessee Coal, Iron & Railroad Co. (U.S. Dept. of Commerce, National Bureau of Standards :, 1942), by Richard S. Dill, Vincent B. Phelan, Ambrose H. Stang, Herbert L. Whittemore, United States. National Bureau of Standards, and Iron & Railroad Co Tennessee Coal (page images at HathiTrust)
• Measurements of heat losses from slab floors (U.S. Dept. of Commerce, National Bureau of Standards :, 1945), by Richard S. Dill, Henry E. Robinson, William C. Robinson, and United States. National Bureau of Standards (page images at HathiTrust)
• Effect of edge insulation upon temperature and condensation on concrete-slab floors (U.S. Dept. of Commerce, National Bureau of Standards :, 1953), by Harold R. Martin, Richard S. Dill, Paul R. Achenbach, and United States. National Bureau of Standards (page images at HathiTrust)
• Calibration of time response of thermometers : concepts and model calculations (Dept. of Commerce National Bureau of Standards :, 1978), by Raymond D. Mountain, G. W. Mulholland, Institute for Applied Technology (U.S.), and Institute for Basic Standards (U.S.) (page images at HathiTrust)
• Heat transfer lectures [given at the NEPA heat transfer symposium ... December 8-13, 1947] (Oak Ridge : [publisher not identified], 1948-, 1947), by Oak Ridge Fairchild Engine and Airplane Corporation. Nuclear Energy Power for Aircraft Division (page images at HathiTrust; US access only)
• Gasdynamic theory of heat (Headquarters, Air Materiel Command, Wright-Patterson Air Force Base, 1949), by L. E. Kalikhman (page images at HathiTrust)
• Heat transfer in noncircular ducts. (Technical Information Service, 1951), by H. C. Claiborne (page images at HathiTrust)
• Liepmann's heat transfer method in aerothermochemistry. (Purdue University, School of Aeronautical Engineering, 1959), by Robert Goulard (page images at HathiTrust)
• High temperature heat transfer gages; high temperature thin-film resistance thermometers for heat transfer measurements. (Cornell Aeronautical Laboratory, Inc., 1963), by L. Bogdan and Cornell Aeronautical Laboratory (page images at HathiTrust)
• A summary of research in diabatic flow (Purdue University, School of Aeronautical Engineering, 1957), by H. M. Degroff, L. A. Hromas, and R. J. Goulard (page images at HathiTrust)
• An experimental study of the operating characteristics and electrode heat transfer of a direct current electric arc in a pressurized argon environment (Purdue University, School of Aeronautical Engineering, 1959), by George M. Palmer and Frank L. Paris (page images at HathiTrust)
• Heat transfer rates for cross flow of water through a tube bank at high Reynolds numbers. (Brookhaven National Laboratory, 1952), by O. E. Dwyer (page images at HathiTrust)
• Effect of geographical variation on performance of recirculating cooling ponds (Corvallis, Oregon : National Environmental Research Center, Office of Research and Development, U.S. Environmental Protection Agency, 1974., 1974), by Edward L. Thackston, Vanderbilt University. Department of Environmental and Water Resources Engineering, Or.) National Environmental Research Center (Corvallis, and United States. Environmental Protection Agency. Office of Research and Development (page images at HathiTrust)
• Heat transfer and fluid flow; a compilation. (National Aeronautics and Space Administration, Technology Utilization Division; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1968), by United States. National Aeronautics and Space Administration. Technology Utilization Division (page images at HathiTrust; US access only)
• Thermal radiation heat transfer (Scientific and Technical Information Division, National Aeronautics and Space Administration; [for sale by the Supt. of Docs., U.S. Govt. Print. Off.], 1968), by Robert Siegel and John R. Howell (page images at HathiTrust; US access only)
• Heat transfer from a gas stream to a bed of broken solids (U.S. G.P.O., 1932), by C. C. Furnas (page images at HathiTrust)
• NASA TT F-262 (National Aeronautics and Space Administration ;, 1965), by M. M. Nazarchuk, M. M. Nazarchuk, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Forced-flow once-through boilers : NASA research (Scientific and Technical Information Office, National Aeronautics and Space Administration ;, 1975), by James R. Stone, Vernon H Gray, Orlando A Gutierrez, and Lewis Research Center (page images at HathiTrust)
• Natural convection heat transfer in boiling of metals / by V. N. [i.e. I.] Subbotin ... [et al.]. (National Aeronautics and Space Administration ;, 1971), by V. I. Subbotin (page images at HathiTrust; US access only)
• Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by Kenneth J. Kacynski, Tamara A. Smith, Albert J. Pavli, and Lewis Research Center (page images at HathiTrust)
• Heat transfer in the atmosphere. (National Aeronautics and Space Administration, 1974), by E. M. Feĭgelʹson, Eva Mikhaĭlovna Feigel'son, and L. R. T︠S︡vang (page images at HathiTrust; US access only)
• Application of turbulence modeling to predict surface heat transfer in stagnation flow region of circular cylinder (National Aeronautics and Space Administration, 1987), by Chi R. Wang, Frederick C. Yeh, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic pressures and heating rates on surfaces between split elevons at Mach 6.6 (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by L. Roane Hunt and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Effect of the radiant heat component on heat transfer in vacuum sublimation (National Aeronautics and Space Administration, 1963), by P. A. Novikov, United States National Aeronautics and Space Administration, and Faraday Translations (page images at HathiTrust)
• A review of high-speed, convective, heat-transfer computation methods (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989), by Michael E. Tauber and United States. National Aeronautics and Space Administration. Office of Management (page images at HathiTrust)
• Surface flow and heating distributions on a cylinder in near wake of Aeroassist Flight Experiment (AFE) configuration at incidence in Mach 10 air (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by William L. Wells and Langley Research Center (page images at HathiTrust)
• Numerical study of shock-induced combustion in methane-air mixtures (National Aeronautics and Space Administration ;, 1993), by Shaye Yungster, Martin J. Rabinowitz, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A p-version finite element method for steady incompressible fluid flow and convective heat transfer (National Aeronautics and Space Administration ;, 1993), by Daniel Winterscheidt and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The effect of protuberances, cavities, and angle of attack on the wind-tunnel pressure and heat-transfer distribution for the Apollo command module (National Aeronautics and Space Administration ;, 1966), by John J. Bertin and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Effects of a ceramic coating on metal temperatures of an air-cooled turbine vane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Herbert J. Gladden, Curt H. Liebert, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Experimental study of effect of simulated reactor core position on nozzle heat transfer (National Aeronautics and Space Administration ;, 1966), by James F. Schmidt and Lewis Research Center (page images at HathiTrust)
• Extension of similarity test procedures to cooled engine components with insulating ceramic coatings (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Herbert J. Gladden, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Vacuum chamber heat-transmission analysis (National Aeronautics and Space Administration ;, 1967), by Walter W. Guy, Wilbert E. Ellis, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Reduction method for thermal analysis of complex aerospace structures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Charles P. Shore, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Visualization techniques to experimentally model flow and heat transfer in turbine and aircraft flow passages (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), by Louis M. Russell and Steven A. Hippensteele (page images at HathiTrust)
• Crossflow effects on impingement cooling of a turbine vane (National Aeronautics and Space Administration ;, 1974), by James W. Gauntner and Lewis Research Center (page images at HathiTrust)
• Experimental investigation at Mach 8 of the effects of projections and cavities on heat transfer to a model of the Viking aeroshell (National Aeronautics and Space Administration ;, 1974), by Theodore R. Creel and Langley Research Center (page images at HathiTrust)
• Finite-element reentry heat-transfer analysis of space shuttle orbiter (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by William L. Ko, Leslie Gong, Robert D. Quinn, and Ames Research Center (page images at HathiTrust)
• Aerothermal evaluation of a spherically blunted body with a trapezoidal cross section in the Langley 8-foot high-temperature tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by Cindy W. Albertson and Langley Research Center (page images at HathiTrust)
• Theoretical study of nonadiabatic boundary-layer stabilization times in a cryogenic wind tunnel for typical stainless-steel wing and fuselage models (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Charles B. Johnson, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Aerodynamic characteristics at low Reynolds numbers of several heat-exchanger configurations for wind-tunnel use (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by William G. Johnson, William B. Igoe, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Heat transfer distributions induced by elevon deflections on swept wings and adjacent surfaces at Mach 6 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Charles B. Johnson, Louis G. Kàufman, Grumman Aerospace Corporation, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Review and status of heat-transfer technology for internal passages of air-cooled turbine blades (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Frederick C. Yeh, Francis S. Stepka, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Water table tests of proposed heat transfer tunnels for small turbine vanes (National Aeronautics and Space Administration ;, 1974), by Peter L. Meitner and Lewis Research Center (page images at HathiTrust)
• Laminar heat-transfer distributions on biconics at incidence in hypersonic-hypervelocity flows (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Charles G. Miller, Peter A. Gnoffo, John R. Micol, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A cascade investigation of a convection- and film-cooled turbine vane made from radially stacked laminates (National Aeronautics and Space Administration ;, 1974), by Herbert J. Gladden and Lewis Research Center (page images at HathiTrust)
• Comparison of thin-film resistance heat-transfer gages with thin-skin transient calorimeter gages in conventional hypersonic wind tunnels (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Charles G. Miller, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Heat-transfer and pressure measurements on a simulated elevon deflected 30 ̊near flight conditions at Mach 7 (National Aeronautics and Space Administration ;, 1977), by Charles B. Johnson, Irving Weinstein, Allan H. Taylor, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of metal temperature and coolant flow with a thermal-barrier coating on a full-coverage-film-cooled turbine vane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Peter L. Meitner, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Propulsion Laboratory (U.S.) (page images at HathiTrust)
• Configuration heating for a hypersonic research airplane concept having a 70 ̊swept double-delta wing (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Pierce L. Lawing and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• One-dimensional numerical analysis of the transient thermal response of multilayer insulative systems (U.S. National Aeronautics and Space Administration ;, 1976), by C. M. Pittman, Kay L. Brinkley, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Optimum element density studies for finite-element thermal analysis of hypersonic aircraft structures (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by William L. Ko, Kyle M. Muramoto, Timothy Olona, and Dryden Flight Research Facility (page images at HathiTrust)
• Heat-transfer distributions on a 0.013-scale shuttle solid rocket booster at Mach 3.70 and angles of attack from 0 ̊to 180 ̊ (National Aeronautics and Space Administration ;, 1976), by Milton Lamb, Robert L. Stallings, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind tunnel investigation of simulated helicopter engine exhaust interacting with windstream (National Aeronautics and Space Administration ;, 1974), by Craig S. Shaw, John C. Wilson, and Langley Research Center (page images at HathiTrust)
• Metal temperatures and coolant flow in a wire-cloth transpiration-cooled turbine vane (National Aeronautics and Space Administration ;, 1975), by Herbert J. Gladden (page images at HathiTrust)
• Turbine vane coolant flow variations and calculated effects on metal temperatures (National Aeronautics and Space Administration ;, 1975), by Frederick C. Yeh, Louis M. Russell, Peter L. Meitner, and Lewis Research Center (page images at HathiTrust)
• Method of predicting radiation heat transfer in turbine-cooling test facilities (National Aeronautics and Space Administration ;, 1975), by Herbert J. Gladden, Curt H. Liebert, and Lewis Research Center (page images at HathiTrust)
• Surface heat-transfer coefficients of pin-finned cylinders (National Aeronautics and Space Administration ;, 1975), by G. James VanFossen, U.S. Army Air Mobility Research and Development Laboratory, and Lewis Research Center (page images at HathiTrust)
• Aerodynamic performance of a fully film cooled core turbine vane tested with cold air in a two-dimensional cascade (National Aeronautics and Space Administration ;, 1975), by Roy G. Stabe, John F. Kline, and Lewis Research Center (page images at HathiTrust)
• Description and orbit data of variable-conductance heat-pipe system for the communications technology satellite (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Louis Gedeon, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Experimental and predicted heating distributions for biconics at incidence in air at Mach 10 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Charles G. Miller and Langley Research Center (page images at HathiTrust)
• Emittance and absorptance of NASA ceramic thermal barrier coating system (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Curt H. Liebert and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• A numerical solution of the Navier-Stokes equations for chemically nonequilibrium, merged stagnation shock layers on spheres and two-dimensional cylinders in air (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Kenneth D. Johnston and William L. Hendricks (page images at HathiTrust)
• Aerodynamic heating on the corrugated surface of a 10.2⁰ half-angle blunted cone at Mach 6.7 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Irving Weinstein, L. Roane Hunt, Don E. Avery, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Robert D. Quinn, Leslie Gong, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by William D. Deveikis and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Influence of thermal boundary conditions on heat transfer from a cylinder in crossflow (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by S. Stephen Papell, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Heat-transfer characteristics of partially film coded plug nozzle on a J-85 afterburning turbojet engine (U.S. National Aeronautics and Space Administration ;, 1976), by Stanley M. Nosek, David M. Straight, and Lewis Research Center (page images at HathiTrust)
• A feasibility study of heat-pipe-cooled leading edges for hypersonic cruise aircraft (National Aeronautics and Space Administration, 1971), by Calvin C. Silverstein, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental study of multi-component coaxial-flow jets in short chambers (National Aeronautics and Space Administration, 1968), by Bruce V. Johnson (page images at HathiTrust; US access only)
• An investigation of the high speed turbulent boundary layer with heat transfer and arbitrary pressure gradient (National Aeronautics and Space Administration ;, 1970), by Constantino Economos, J. L. Boccio, Langley Research Center, and Nassau County General Applied Science Laboratories (Westbury (page images at HathiTrust)
• Transient radiation and conduction in a slotted slab and a hollow cylinder (National Aeronautics and Spac Administration]; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1967), by Peter Damian Richardson, Y. M. Shum, and Brown University (page images at HathiTrust; US access only)
• Heat transfer on a flat plate in continuum to rarefied hypersonic flows at Mach numbers of 19.2 and 25.4 (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by Henry T. Nagamatsu, R. E. Sheer, W. T. Pettit, and General Electric Company. Research and Development Center (page images at HathiTrust; US access only)
• A study of boundary layer transition on outgassing cones in hypersonic flow (National Aeronautics and Space Administration, 1971), by C. J. Stalmach, United States National Aeronautics and Space Administration, Vought Aeronautics Company, and Langley Research Center (page images at HathiTrust)
• Stagnation point heat transfer during hypervelocity atmospheric entry (National Aeronautics and Space Administration ;, 1970), by W. S. Rigdon, M. Thomas, R. B. Dirling, McDonnell Douglas Astronautics Company. Western Division, and Langley Research Center (page images at HathiTrust)
• Study of a heat rejection system using capillary pumping (National Aeronautics and Space Administration ;, 1971), by L. G. Neal, O. W. Clausen, D. J. Wanous, Lewis Research Center, and TRW Systems Group (page images at HathiTrust)
• Calculation of turbulent boundary layers with heat transfer and pressure gradient utilizing a compressibility transformation. Part 1, Summary report (National Aeronautics and Space Administration ;, 1971), by C. Economos, J. Boccio, Langley Research Center, and Nassau County General Applied Science Laboratories (Westbury (page images at HathiTrust)
• Calculation of turbulent boundary layers with heat transfer and pressure gradient utilizing a compressibility transformation. Part III, Computer program manual (National Aeronautics and Space Administration ;, 1972), by J. Schneider, J. Boccio, Langley Research Center, and Nassau County General Applied Science Laboratories (Westbury (page images at HathiTrust)
• Potassium rankine cycle vapor chamber (heat pipe) radiator study (National Aeronautics and Space Administration ;, 1971), by Ellsworth E. Gerrels, Robert E. Killen, Lewis Research Center, and General Electric Company (page images at HathiTrust)
• Vapor condensing at high velocities ... (National Aeronautics and Space Administration, 1964), by Winthrop E. Hilding, Charles H. Coogan, University of Connecticut, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Measurements of nonequilibrium effects in air on wedge-flat-plate afterbody pressures (National Aeronautics and Space Administration, 1965), by R. J. Vidal and F. Stoddard (page images at HathiTrust; US access only)
• Integral methods in compressible laminar boundary layers and their application to hypersonic pressure interactions (National Aeronautics and Space Administration, 1965), by Yat-Yung Chan (page images at HathiTrust; US access only)
• Experimental determination of transport properties of high temperature gases (National Aeronautics and Space Administration, 1967), by E. H. Carnevale (page images at HathiTrust; US access only)
• Convective and radiative heat transfer during superorbital entry (National Aeronautics and Space Administration, 1966), by H. Hoshizaki and K. H. Wilson (page images at HathiTrust; US access only)
• Turbulent boundary layer on a full-coverage film-cooled surface : an experimental heat transfer study with normal injection (National Aeronautics and Space Administration ;, 1976), by H. Choe, R. J. Moffat, W. M. Kays, and Stanford University (page images at HathiTrust)
• Heat pipes (National Aeronautics and Space Administration, 1975), by United States National Aeronautics and Space Administration and Mo.) Midwest Research Institute (Kansas City (page images at HathiTrust)
• Full-coverage film cooling heat transfer study : summary of data for normal-hole injection and 30 ̊slant-hole injection (U.S. National Aeronautics and Space Administration ;, 1976), by M. E. Crawford, Lewis Research Center, Stanford University, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Heat transfer to a full-coverage film-cooled surface with 30 ̊slant-hole injection (National Aeronautics and Space Administration ;, 1976), by M. E. Crawford, R. J. Moffat, W. M. Kays, Stanford University, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Stability of a plane vortex sheet between gases exchanging heat by radiation (National Aeronautics and Space Administration, 1971), by Burton E. Eno, Cornell University, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Observation of flow excursions in a simulated gas-cooled reactor passage (National Aeronautics and Space Administration ;, 1970), by Paul Vingerhoet, Eli Reshotko, Edward R. Kolbe, Lewis Research Center, and Case Western Reserve University (page images at HathiTrust)
• Dynamic response of high-frequency pressure transducers to large amplitude sinusoidal pressure oscillations (National Aeronautics and Space Administration ;, 1972), by Richard E. Robinson, Lewis Research Center, and Battelle Memorial Institute (page images at HathiTrust)
• Subcooled forced convection boiling of trichlorotrifluoroethane (National Aeronautics and Space Administration ;, 1972), by R. S. Dougall, D. J. Panian, Lewis Research Center, and University of Pittsburgh (page images at HathiTrust)
• Jet array impingement with crossflow - correlation of streamwise resolved flow and heat transfer distributions (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by L. W. Florschuetz, C. R. Truman, Darryl E. Metzger, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Heat and mass transfer at a general three-dimensional stagnation point (National Aeronautics and Space Administration, 1967), by Paul A. Libby (page images at HathiTrust; US access only)
• Heat transfer coefficients of dilute flowing gas-solids suspensions (National Aeronautics and Space Administration ;, 1973), by Ronald S. Kane, Robert Pfeffer, Lewis Research Center, and City University of New York (page images at HathiTrust)
• Extended hydrodynamic theory of the peak and minimum pool boiling heat fluxes (National Aeronautics and Space Administration ;, 1973), by John H. Lienhard, V. K. Dhir, Lewis Research Center, and University of Kentucky (page images at HathiTrust)
• Thermal and hydraulic performance of potassium during condensation inside single tubes (National Aeronautics and Space Administration, 1967), by S. G. Sawochka (page images at HathiTrust; US access only)
• Turbulent boundary layer heat transfer experiments : convex curvature effects including introduction and recovery (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by T. W. Simon, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Effects of unsteady free stream velocity and free stream turbulence on stagnation point heat transfer (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Rama S. R. Gorla, Cleveland State University, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
• Application of the Hughes-Liu algorithm to the two-dimensional heat equation / David S. Malkus and Peter I. Reichmann, Raphael T. Haftka ; prepared for Langley Research Center under grant NAG1-224 and NSG-1266. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by David S. Malkus, Raphael T. Haftka, Peter I. Reichmann, Virginia Polytechnic Institute and State University. Aerospace and Ocean Engineering Dept, Illinois Institute of Technology. Dept. of Mathematics, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Jet array impingement flow distributions and heat transfer characteristics : effects of initial crossflow and nonuniform array geometry (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by L. W. Florschuetz, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
• On the question of instabilities upstream of cylindrical bodies (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Mark V. Morkovin, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Multiple jet impingement heat transfer characteristic : experimental investigation of in-line and staggered arrays with crossflow (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by L. W. Florschuetz, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Full-coverage film cooling on flat, isothermal surfaces : a summary report on data and predictions (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by M. E. Crawford, R. J. Moffat, W. M. Kays, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Effects of mach number and wall-temperature ratio on turbulent heat transfer at mach numbers from 3 to 5 (U.S. G.P.O.], 1959), by Thorval Tendeland (page images at HathiTrust)
• NASA TR R-142 (National Aeronautics and Space Administration ;, 1962), by Charles E. Feiler, Ernest B. Yeager, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Mass transfer cooling near the stagnation point (U.S. G.P.O., 1959), by Leonard Roberts, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• A Theoretical study of stagnation-point ablation (U.S. G.P.O., 1959), by Leonard Roberts, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Stagnation-point shielding by melting and vaporization (U.S. G.P.O., 1959), by Leonard Roberts, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• NASA TR R-295 (National Aeronautics and Space Administration ;, 1968), by Walter B. Olstad, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Heat transfer and pressure drop in blade cooling channels with turbulence promoters (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by J. C. Han, C. K. Lei, J. S. Park, Lewis Research Center, and Texas A & M University. Dept. of Mechanical Engineering (page images at HathiTrust)
• Thermotransport in liquid aluminum-copper alloys (National Aeronautics and Space Administration ;, 1973), by B. N. Bhat and George C. Marshall Space Flight Center (page images at HathiTrust)
• On the temperature distribution behind cylinders in a flow (National Aeronautics and Space Administration, 1959), by Ackeret Jakob and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Analysis of thermal-protection systems for space-vehicle cryogenic-propellant tanks (U.S. G.P.O., 1962), by George R. Smolak, Lewis E. Wallner, Richard H. Knoll, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-1987 (National Aeronautics and Space Administration, 1963), by Morris Perlmutter, John R. Howell, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Heat transfer with laminar flow in concentric annuli with constant and variable wall temperature and heat flux (National Aeronautics and Space Administration, 1963), by Raymond Eugene Lundberg, W. M. Kays, William Craig Reynolds, Stanford University, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Convective heat transfer in planetary gases (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1965), by Joseph G. Marvin and George S. Deiwert (page images at HathiTrust; US access only)
• Use of fusible temperature indicators for obtaining quantitative aerodynamic heat-transfer data (U.S. National Aeronautics and Space Administration, 1966), by Robert A. Jones and James L. Hunt (page images at HathiTrust; US access only)
• NASA TN D-2077 (National Aeronautics and Space Administration, 1963), by E. M. Sparrow, W. J. Minkowycz, V. Jonsson, University of Minnesota, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Pressure gradient effects on heat transfer to reusable surface insulation tile-array gaps (National Aeronautics and Space Administration ;, 1975), by David A. Throckmorton and Langley Research Center (page images at HathiTrust)
• Evaluation of shock-tube heat-transfer experiments to measure thermal conductivity of argon from 700 ̊to 8600 ̊K (National Aeronautics and Space Administration :, 1964), by Milton R. Lauver and Lewis Research Center (page images at HathiTrust)
• Experimental heat transfer and pressure drop of liquid hydrogen flowing through a heated tube (National Aeronautics and Space Administration, 1961), by Robert C. Hendricks and Lewis Research Center (page images at HathiTrust)
• NASA TN D-2511 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1964), by Jay Fox, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-2411 (National Aeronautics and Space Administration :, 1964), by Joseph M. Savino, Edward C. Bittner, Robert Siegel, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust; US access only)
• Analysis of the transient radiation heat transfer of an uncooled rocket engine operating outside Earth's atmosphere (National Aeronautics and Space Administration, 1959), by William H. Robbins and Lewis Research Center (page images at HathiTrust)
• NASA TN D-3571 (National Aeronautics and Space Administration :, 1966), by Charles W. McKee and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Laminar heat-transfer and pressure measurements at a Mach number of 6 on a sharp and blunt 15° half-angle cones at angles of attack up to 90° (National Aeronautics and Space Administration, 1961), by Raul J. Conti, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• NASA TN D-4035 (National Aeronautics and Space Administration ;, 1967), by Kenneth J. Baumeister, Thomas D. Hamill, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5121 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by James C. Ellison, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5251 (National Aeronautics and Space Administration ;, 1969), by James L. Hunt, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Approximation for radiant energy transport in nongray, nonscattering gases (National Aeronautics and Space Administration ;, 1967), by R. W. Patch (page images at HathiTrust)
• The design and uncertainty analysis of an improved total hemispherical emittance transient calorimeter (National Aeronautics and Space Administration ;, 1969), by William R. Wade, Donald J. Progar, and Langley Research Center (page images at HathiTrust)
• NASA TN D-4070 (National Aeronautics and Space Administration ;, 1967), by Thomas H. Cochran, John C. Aydelott, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4065 (National Aeronautics and Space Administration ;, 1967), by Ronald C. Smith, Alan D. Levin, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Planck functions and integrals: methods of computation (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1968), by Thomas E. Michels (page images at HathiTrust; US access only)
• NASA TN D-5168 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Ronald G. Huff, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4057 (National Aeronautics and Space Administration ;, 1967), by James R. Stone, Thomas M. Damman, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4907 (National Aeronautics and Space Administration :, 1968), by James P. Arrington, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Turbulent heat-transfer prediction method for application to scramjet engines (National Aeronautics and Space Administration ;, 1974), by S. Z. Pinckney and Langley Research Center (page images at HathiTrust)
• Comparison of predicted and experimental wall temperatures for a cylindrical ejector exhaust nozzle operated with a turbojet gas generator (National Aeronautics and Space Administration, 1971), by Arthur Lieberman, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6192 (National Aeronautics and Space Administration ;, 1971), by Ivan E. Beckwith, Frank L. Clark, William D. Harvey, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Combined radiation, convection, and conduction for a system with a partially transmitting wall (National Aeronautics and Space Administration ;, 1975), by Robert Siegel, Nihad A. Hussain, and Lewis Research Center (page images at HathiTrust)
• Steady-state heat transfer in transversely heated porous media with application to focused solar energy collectors (National Aeronautics and Space Administration ;, 1976), by Lester D. Nichols, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6160 (National Aeronautics and Space Administration :, 1971), by Francis C. Chenoweth (page images at HathiTrust; US access only)
• Nonlinear decay of a disturbance in an unbounded viscous fluid (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1968), by Robert G. Deissler (page images at HathiTrust; US access only)
• Shock interference heat transfer to tank configurations mated to a straight-wing space shuttle orbiter at mach number 10.3 (National Aeronautics and Space Administration ;, 1976), by Davis H. Crawford, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• A simplified analytical solution for thermal response of a one-dimensional, steady-state transpiration cooling system in radiative and convective environment (National Aeronautics and Space Administration ;, 1976), by Hirotoshi Kubota and Ames Research Center (page images at HathiTrust)
• NASA TN D-6152 (National Aeronautics and Space Administration ;, 1971), by Alden F. Presler, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5863 (National Aeronautics and Space Administration :, 1970), by Aubrey M. Cary, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Survey of heat transfer to near-critical fluids (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by Robert C. Hendricks, Ray V. Smith, and Robert J. Simoneau (page images at HathiTrust; US access only)
• Heat-transfer coefficients for hydrogen flowing through parallel hexagonal passages at surface temperatures to 2275 K (National Aeronautics and Space Administration ;, 1968), by Jack G. Slaby, William F. Mattson, and Lewis Research Center (page images at HathiTrust)
• Streakline flow visualization of discrete-hole film cooling with normal, slanted and compound angle injection (National Aeronautics and Space Administration ;, 1976), by Raymond S. Colladay, Louis M. Russell, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Heat-transfer characteristics of a water-to-cryogenic-hydrogen heat exchanger (National Aeronautics and Space Administration ;, 1969), by Walter F. Weiland, Donald W. Adams, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-5887 (National Aeronautics and Space Administration :, 1970), by Meyer Reshotko, Robert C. Ehlers, Donald R. Boldman, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flow and heat transfer in a curved channel (National Aeronautics and Space Administration ;, 1977), by Paul F. Brinich and Robert W. Graham (page images at HathiTrust)
• NASA TN D-5899 (National Aeronautics and Space Administration :, 1970), by Charles B. Johnson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5908 (National Aeronautics and Space Administration :, 1970), by Allan R. Wieting, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Analytical heat transfer investigation of insulated liquid methane wing tanks for supersonic cruise aircraft (National Aeronautics and Space Administration :, 1970), by Eugene J. Pleban, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Survey of literature on flow characteristics of a single turbulent jet impinging on a flat plate. (National Aeronautics and Space Administration :, 1970), by James W. Gauntner, Peter Hrycak, John N. B. Livingood, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5694 (National Aeronautics and Space Administration :, 1970), by Robert C. Hendricks, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5418 (National Aeronautics and Space Administration ;, 1969), by J. Wayne Keyes, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Calculation of laminar heat transfer to the windward surfaces of straight wing shuttle vehicles at high angle of attack and with yaw (National Aeronautics and Space Administration ;, 1972), by C. C. Pappas, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Analysis of heat transfer in a porous cooled wall with variable pressure and temperature along the coolant exit boundary (National Aeronautics and Space Administration ;, 1972), by Robert Siegel, Marvin E. Goldstein, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-5356 (National Aeronautics and Space Administration ;, 1969), by Robert W. Graham, Donald R. Boldman, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The influence of low wall temperature on boundary-layer transition and local heat transfer on 2-inch-diameter hemispheres at a Mach number of 4.95 and a Reynolds number per foot of 73.2 x 10⁶ (National Aeronautics and Space Administration, 1960), by Morton Cooper, Jerome D. Julius, Edward E. Mayo, and Langley Research Center (page images at HathiTrust)
• Heat transfer to cylinders in crossflow in hypersonic rarefied gas streams (National Aeronautics and Space Administration, 1960), by Ruth N. Weltmann, Perry W. Kuhns, and Lewis Research Center (page images at HathiTrust)
• Supersonic free-flight measurements of heat transfer and transition on a 10° cone having a low temperature ratio (National Aeronautical and Space Administration, 1961), by Charles F. Merlet, Charles B. Rumsey, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Free flight observation of a separated turbulent flow including heat transfer up to Mach 8.5 (National Aeronautics and Space Administration, 1960), by Dudley George McConnell and Lewis Research Center (page images at HathiTrust)
• Effect of geometry variations on lee-surface vortex-induced heating for flat-bottom three-dimensional bodies at Mach 6 (National Aeronautics and Space Administration ;, 1973), by Jerry N. Hefner and Lanley Research Center (page images at HathiTrust)
• A visual technique for determining qualitative aerodynamic heating rates on complex configurations (National Aeronautics and Space Administration :, 1960), by P. Calvin Stainback and Langley Research Center (page images at HathiTrust)
• Zero- and reduced-gravity simulation on a magnetic-colloid pool-boiling system (National Aeronautics and Space Administration ;, 1966), by S. Stephen Papell, Otto C. Faber, and Lewis Research Center (page images at HathiTrust)
• Heat-transfer and pressure distributions for laminar separated flows downstream of rearward-facing steps with and without mass suction (National Aeronautics and Space Administration ;, 1974), by Ronald D. Brown, Antoni K. Jakubowski, and Langley Research Center (page images at HathiTrust)
• NASA TN D-4671 (National Aeronautics and Space Administration ;, 1968), by William D. Harvey, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An exact closed-form solution for constant-area compressible flow with friction and heat transfer (National Aeronautics and Space Administration ;, 1971), by Jonas I. Sturas, United States. National Aeronautical and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Effects of wall cooling and angle of attack on boundary-layer transition on sharp cones at M[mathematical symbol for infinity] = 7.4 (National Aeronautics and Space Administration ;, 1972), by George G. Mateer, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Heat transfer to 0 degree and 75 degree swept blunt leading edges in free flight at mach numbers from 1.90 to 3.07. Robert L. O'Neal and Aleck C. Bond. (National Aeronautics and Space Administration :, 1962), by Robert L. O'Neal, Aleck C. Bond, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Minimum film-boiling heat flux in vertical flow of liquid nitrogen (National Aeronautics and Space Administration ;, 1968), by Frederick F. Simon, Robert J. Simoneau, S. Stephen Papell, and Lewis Research Center (page images at HathiTrust)
• Experimental heat-transfer study of a regeneratively cooled hydrogen-fluorine rocket engine at low chamber pressure (National Aeronautics and Space Administration ;, 1967), by Arthur N. Curren and Lewis Research Center (page images at HathiTrust)
• NASA TN D-2556 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1964), by Carol J. Sotos, Norbert O. Stockman, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Energy transfer from a liquid to gas bubbles forming at a submerged orifice (National Aeronautics and Space Administration :, 1965), by M. R. L'Ecuyer, S. N. B. Murthy, United States National Aeronautics and Space Administration, and Purdue University. Jet Propulsion Center (page images at HathiTrust)
• Afterbody heating data obtained from an atlas-boosted mercury configuration in a free body reentry (National Aeronautics and Space Administration, 1961), by Emily W. Stephens and United States. National Aeronautics and Space Administration. Space Task Group (page images at HathiTrust)
• Convective heat transfer to a lifting flat-faced-cone entry body (National Aeronautics and Space Administration, 1961), by James E. Terry and Ames Research Center (page images at HathiTrust)
• NASA TN D-6405 (National Aeronautics and Space Administration:, 1971), by Raymond S. Colladay (page images at HathiTrust; US access only)
• NASA D-3230 (National Aeronautics and Space Administration :, 1966), by Alden F. Presler, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-1874 (National Aeronautics and Space Administration, 1963), by John R. Howell, Morris Perlmutter, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-6450 (National Aeronautics and Space Administration :, 1971), by William R. Jones, Lavern D. Wedeven, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental performance of an internal resistance heater for Langley 6-inch expansion tube driver (National Aeronautics and Space Administration ;, 1972), by Thomas R. Creel and Langley Research Center (page images at HathiTrust)
• Reliability and effective thermal conductivity of three metallic-ceramic composite insulating coatings on cooled hydrogen-oxygen rockets (National Aeronautics and Space Administration ;, 1973), by Harold G. Price, Richard J. Quentmeyer, Ralph L. Schacht, and Lewis Research Center (page images at HathiTrust)
• Experimental study of sharp- and blunt-nose streamwise corners at Mach 20 (National Aeronautics and Space Administration ;, 1974), by Ralph D. Watson and Langley Research Center (page images at HathiTrust)
• NASA TN D-6402 (National Aeronautics and Space Administration:, 1971), by James R. Stone (page images at HathiTrust; US access only)
• Analytical and experimental study of pool heating of liquid hydrogen over a range of accelerations (National Aeronautics and Space Administration :, 1965), by Robert W. Graham, Robert C. Ehlers, Robert C. Hendricks, and Lewis Research Center (page images at HathiTrust)
• Similar solutions for turbulent boundary layer with large favorble pressures gradients (nozzle flow with heat transfer) (National Aeronautics and Space Administration, 1971), by James F. Schmidt, Carroll Todd, Donald R. Boldman, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• The influence of heating rate and test stream oxygen content on the insulation efficiency of charring materials (National Aeronautics and Space Administration :, 1963), by Nick S. Vojvodich, Ernest L. Winkler, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Measurement of the heat transfer to bodies of revolution in free flight by use of a catcher calorimeter (National Aeronautics and Space Administration :, 1963), by Gary T. Chapman, Charles T. Jackson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6422 (National Aeronautics and Space Administration ;, 1971), by Ronald G. Huff, Frank B. Molls, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Two-dimensional analysis of heat and mass transfer in porous media using the strongly implicit procedure (National Aeronautics and Space Administration ;, 1974), by Donald M. Curry and Lyndon B. Johnson Space Center (page images at HathiTrust)
• NASA TN D-6433 (National Aeronautics and Space Administration ;, 1971), by David A. Stewart, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-6307 (National Aeronautics and Space Administration:, 1971), by P. J. Marto (page images at HathiTrust; US access only)
• NASA TN D-4579 (National Aeronautics and Space Administration ;, 1968), by Morris Perlmutter, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental investigation of nucleate boiling bubble dynamics in normal and zero gravities (National Aeronautics and Space Administration ;, 1968), by Thomas H. Cochran, Charles M. Spuckler, John C. Aydelott, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-3779 (National Aeronautics and Space Administration :, 1967), by Robert G. Deissler and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Experimental study of subcooled nucleate boiling of water flowing in 1/4-inch-diameter tubes at low pressures (National Aeronautics and Space Administration :, 1965), by Frank A. Jeglic, Vernon H. Gray, James R. Stone, and Lewis Research Center (page images at HathiTrust)
• Investigation of the flow over a spiked-nose hemisphere-cylinder at a Mach number of 6.8 (National Aeronautics and Space Administration, 1959), by Davis H. Crawford and Langley Research Center (page images at HathiTrust)
• Experimental investigation of metal temperatures of air-cooled airfoil leading edges at subsonic flow and gas temperatures up to 2780 degrees F (National Aeronautics and Space Administration :, 1959), by Francis S. Stepka, Hadley T. Richards, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• FREE-FLIGHT AERODYNAMIC-HEATING DATA TO MACH NUMBER 10.4 FOR A MODIFIED VON KARMAN NOSE SHAPE. (Defense Technical Information Center, 1961), by COLLIE,KATHERINE A, BLAND,WILLIAM M JR, and NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C. (page images at HathiTrust; US access only)
• An investigation of heat transfer within regions of separated flow at a Mach number of 6.0 (National Aeronautics and Space Administration ;, 1965), by Paul F. Holloway, Helen S. Creekmore, James R. Sterrett, and Langley Research Center (page images at HathiTrust)
• Experimental heat-transfer results for cryogenic hydrogen flowing in tubes at subcritical and supercritical pressures to 800 pounds per square inch absolute (National Aeronautics and Space Administration ;, 1966), by Robert C. Hendricks and Lewis Research Center (page images at HathiTrust)
• NASA TN D-3998 (National Aeronautics and Space Administration ;, 1967), by Roy A. Lottig, William D. Kenney, Richard W. Vernon, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Local turbulent heat transfer for water in entrance regions of tubes with various unheated starting lengths (National Aeronautics and Space Administration ;, 1965), by James R. Stone and Lewis Research Center (page images at HathiTrust)
• NASA TN D-1743 (National Aeronautics and Space Administration, 1963), by Anthony Fortini, Robert C. Ehlers, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-4722 (National Aeronautics and Space Administration ;, 1968), by Chester D. Lanzo, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Vaporization rates of ethanol sprays in a combustor with low-frequency fluctuations of combustion-gas pressure / Robert D. Ingebo. (National Aeronautics and Space Administration :, 1962), by Robert D. Ingebo and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4543 (National Aeronautics and Space Administration ;, 1968), by Dennis M. Bushnell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Free-flight investigation of heat transfer to an unswept cylinder subjected to an incident shock and flow interference from an upstream body at Mach numbers up to 5.50 (National Aeronautics and Space Administration, 1961), by Howard S. Carter, Robert E. Carr, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• A visual study of two-phase flow in a vertical tube with heat addition (National Aeronautics and Space Administration, 1963), by Yih Yun Hsu, United States National Aeronautics and Space Administration, and Robert W. Graham (page images at HathiTrust)
• Base heat transfer, pressure ratios, and configuration effects obtained on a 1/27 scall saturn (C-1) model at mach numbers from 0.1 to 2.0 (National Aeronautics and Space Administration, 1963), by John L. Allen, Robert A. Wasko, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4514 (National Aeronautics and Space Administration ;, 1968), by Byron L. Siegel, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Empirical equation for turbulent forced-convection heat transfer for prandtl numbers from 0.001 to 1000 (National Aeronautics and Space Administration :, 1960), by Uwe H. VonGlahn and Lewis Research Center (page images at HathiTrust)
• Tables and graphs of functions necessary for solving nonlinear heat transfer constant area fin problems : with examples of their use (National Aeronautics and Space Administration ;, 1968), by Ahmad Raafat Shouman and J. W. Price (page images at HathiTrust)
• Laminar heat-transfer distributions for a blunted-cone, cone-frustum reentry configuration at Mach 10 (National Aeronautics and Space Administration ;, 1969), by J. David Dearing and Langley Research Center (page images at HathiTrust)
• NASA TN D-3486 (National Aeronautics and Space Administration :, 1966), by C. M. Pittman, William D. Brewer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Two techniques for detecting boundary-layer transition in flight at supersonic speeds and at altitudes above 20,000 feet (National Aeronautics and Space Administration, 1959), by John G. McTigue, Gilbert Petty, John D. Overton, and Flight Research Center (U.S.) (page images at HathiTrust)
• Approximate composition and thermodynamic properties of nonionized nitrogen-oxygen mixtures (National Aeronautics and Space Administration, 1959), by Richard A. Hord and Langley Research Center (page images at HathiTrust)
• Curve fits of predicted inviscid stagnation-point radiative heating rates, cooling factors, and shock standoff distances for hyperbolic earth entry (National Aeronautics and Space Administration ;, 1974), by John T. Suttles, Stephen B. Margolis, Edward M. Sullivan, and Langley Research Center (page images at HathiTrust)
• NASA TN D-6228 (National Aeronautics and Space Administration ;, 1971), by Glenn R. Cowgill, William R. Johnson, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-6220 (National Aeronautics and Space Administration ;, 1971), by Stephen S. Tompkins, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Net radiation method for enclosure systems involving partially transparent walls (National Aeronautics and Space Administration ;, 1973), by Robert Siegel and Lewis Research Center (page images at HathiTrust)
• Optical absorption in fused silica at elevated temperatures during 1.5-MeV electron irradiation (National Aeronautics and Space Administration ;, 1972), by Albert B. Smith and Lewis Research Center (page images at HathiTrust)
• Local heat-transfer characteristics of a row of circular air jets impinging on a concave semicylindrical surface (National Aeronautics and Space Administration ;, 1973), by John N. B. Livingood, James W. Gauntner, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Forced-convection peak heat flux on cylindrical heaters in water and refrigerant 113 (National Aeronautics and Space Administration ;, 1974), by Thomas H. Cochran, Charles R. Andracchio, and Lewis Research Center (page images at HathiTrust)
• Heat-transfer and pressure distributions on hemisphere-cylinders in methane-air combustion products at Mach 7 (National Aeronautics and Space Administration ;, 1973), by Irving Weinstein, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Effective thermal conductivities of four metal-ceramic composite coatings in hydrogen-oxygen rocket firings (National Aeronautics and Space Administration ;, 1972), by Ralph L. Schacht, Richard J. Quentmeyer, Harold G. Price, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Analysis of shape of porous cooled medium for an imposed surface heat flux and temperature (National Aeronautics and Space Administration ;, 1973), by Robert Siegel and Lewis Research Center (page images at HathiTrust)
• An analysis of a charring ablator with thermal nonequilibrium, chemical kinetics, and mass transfer (National Aeronautics and Space Administration ;, 1973), by Ronald K. Clark and Langley Research Center (page images at HathiTrust)
• NASA TN D-6594 (National Aeronautics and Space Administration :, 1972), by Donald R. Boldman, Robert W. Graham, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6595 (National Aeronautics and Space Administration :, 1972), by Donald R. Boldman, Robert C. Ehlers, James F. Schmidt, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6331 (National Aeronautics and Space Administration ;, 1971), by Richard L. DeWitt, Max B. Mellner, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Similarity constraints in testing of cooled engine parts (National Aeronautics and Space Administration ;, 1974), by Raymond S. Colladay, Francis S. Stepka, and Lewis Research Center (page images at HathiTrust)
• Numerical and experimental studies of the natural convection within a horizontal cylinder (National Aeronautics and Space Administration ;, 1974), by Roger B. Stewart, Lillian R. Boney, Alexander P. Sabol, and Langley Research Center (page images at HathiTrust)
• Analysis of impingement heat transfer for two parallel liquid-metal slot jets (National Aeronautics and Space Administration ;, 1974), by Robert Siegel and Lewis Research Center (page images at HathiTrust)
• Some characteristics of turbulent boundary layers in rapidly accelerated flows (National Aeronautics and Space Administration ;, 1971), by Paul F. Brinich, Harvey E. Neumann, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Boundary layer measurements in an accelerated flow with and without heat transfer (National Aeronautics and Space Administration ;, 1971), by Howard L. Wesoky, Charlene May, and Lewis Research Center (page images at HathiTrust)
• Coolant-side heat-transfer rates for a hydrogen-oxygen rocket and a new technique for data correlation (National Aeronautics and Space Administration ;, 1973), by Ralph L. Schacht, Richard J. Quentmeyer, and Lewis Research Center (page images at HathiTrust)
• Heat pipe investigations (National Aeronautics and Space Administration ;, 1973), by James P. Marshburn and Goddard Space Flight Center (page images at HathiTrust)
• Heat transfer and thermodynamics. (National Aeronautics and Space Administration. Technology Utilization Office.), by United States. National Aeronautics and Space Administration. Technology Utilization Office (page images at HathiTrust)
• A progress report on theoretical consideration of the heat transfer coefficient (U.S. Atomic Energy Commission, Technical Information Division, 1949), by R. N. Lyon, U.S. Atomic Energy Commission, and Oak Ridge National Laboratory (page images at HathiTrust)
• Heat transfer in stable film boiling. (U.S. Atomic Energy Commission, Technical Information Division, 1949), by LeRoy Alton Bromley, U.S. Atomic Energy Commission, and University of California Radiation Laboratory (page images at HathiTrust)
• Further remarks on the stability of boiling heat transfer (Oak Ridge, Tenn. : Technical Information Service Extension, 1958), by Novak Zuber (page images at HathiTrust)
• Transient heat transfer in reactor coolant channels (Technical Information Service Extension, 1957), by Ralph P. Stein and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heat transfer to molten lead-bismuth eutectic in turbulent pipe flow : July 1, 1951 to February 1,1952 (interim report) (United States Atomic Energy Commission, Technical Information Service, 1952), by H. A. Johnson, W. J. Clabaugh, J. P. Hartnett, and Berkeley. Institute of Engineering Research University of California (page images at HathiTrust)
• Periodic heat transfer by radiation through layers in a vacuum (United States Atomic Energy Commission, Technical Information Service, 1950), by Fred L. Whipple, J. Orten Gadd, Harvard University, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Rate of formation of vapor in a uniformly heated liquid (United States Atomic Energy Commission, Technical Information Service, 1950), by Milton S. Plesset, North American Aviation, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Hydrodynamic aspects of boiling heat transfer (thesis) (United States Atomic Energy Commission, Technical Information Service ;, 1959), by N. Zuber (page images at HathiTrust; US access only)
• The effect of chemical nature of heating surfaces on the heat transfer coefficients of pool boiling liquids : final report for Februrary 1, 1952-June 15, 1955 (United States Atomic Energy Commission, Technical Information Service, 1955), by George William Preckshot, University of Minnesota. Institute of Technology, and U.S. Atomic Energy Commission (page images at HathiTrust)
• The design and operation of a 30 GPM, 40 KW lead-bismuth eutectic heat transfer system (U.S. Atomic Energy Commission. Technical Information Division, 1954), by H. A. Johnson, W. J. Clabaugh, J. P. Hartnett, Berkerley Institute of Engineering Research University of California, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Report on boiling heat transfer (U.S. Atomic Energy Commission. Technical Information Service Extension, 1957), by N. Zuber, Columbia University Heat Transfer Research Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heat equation. (U.S. Atomic Energy Commission. Technical Information Service Extension, 1952), by Richard Bellman, Princeton University, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Progress report no. 2 : heat transfer study of cobalt-60 shipping container (Brookhaven National Laboratory, 1961), by L. B. Adler, Brookhaven National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Turbulent liquid-metal heat transfer in concentric annuli with axially varying heat flux (Brookhaven National Laboratory, 1969), by W. S. Yu, John C. Chen, Brookhaven National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Axial mixing and mass transfer in fused salt-liquid metal extraction columns (Brookhaven National Laboratory, 1963), by F. B. Hill, L. E. Kukacka, Brookhaven National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Progress report no. 1 : heat transfer study of cobalt-60 shipping container (Brookhaven National Laboratory, 1961), by L. B. Adler, Brookhaven National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heat transfer analysis of internally-externally cooled cylindrical fuel elements for nuclear reactors (Hanford Atomic Products Operation, 1954), by F. E. Tippets, General Electric Company, U.S. Atomic Energy Commission, and Hanford Atomic Products Operation (page images at HathiTrust)
• Forced convection heat transfer between parallel plates and in annuli with volume heat sources within the fluids (U.S. Atomic Energy Commission, Technical Information Service, 1954), by H. F. Poppendiek, L. D. Palmer, U.S. Atomic Energy Commission, and Oak Ridge National Laboratory (page images at HathiTrust)
• Reactor Experimental Engineering Division. (Oak Ridge National Laboratory, 1955), by H. F. Poppendiek, L. D. Palmer, U.S. Atomic Energy Commission, and Oak Ridge National Laboratory (page images at HathiTrust)
• Reactor Experimental Engineering Division. (Oak Ridge National Laboratory, 1954), by William B. Harrison, Oak Ridge National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Applications of the finite-element method to the problem of heat transfer in a freezing shaft wall (Cold Regions Research and Engineering Laboratory, 1986), by Fu Liandi, United States Army Corps of Engineers, and Cold Regions Research and Engineering Laboratory (U.S.) (page images at HathiTrust)
• Experimental determination of local and mean coefficients of heat transfer for turbulent flow in pipes (NACA, 1954), by I. T. Aladyev and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Some experiences regarding the nonlinearity of hot wires (NACA, 1952), by Robert Betchov, W. Welling, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Heat transfer, diffusion and evaporation (NACA, 1954), by Wilhelm Nusselt and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Experimental heat-transfer and friction coefficients for air flowing through stacks of parallel flat plates (NACA, 1954), by Eldon W. Sams, Walter F. Weiland, United States National Advisory Committee for Aeronautics, and Lewis Research Center (page images at HathiTrust)
• Some effects of heat transfer at Mach number 2.0 at stagnation temperatures between 2,310À and 3,500À R on a magnesium fin with several leading-edge modifications (NACA, 1957), by W. M. Bland, Walter E. Bressette, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Temperature recovery factors on a slender 12À cone-cylinder at Mach numbers from 3.0 to 6.3 and angles of attack up to 45À (NACA, 1955), by John O. Reller, Frank M. Hamaker, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
• Steam-water condensing-injector performance analysis with supersonic inlet vapor and convergent condensing section (Argonne National Laboratory, Reactor Engineering Division ;, 1968), by M. A. Grolmes, U.S. Atomic Energy Commission, and Argonne National Laboratory (page images at HathiTrust)
• Heat transfer to boiling water forced through a uniformly heated tube (Argonne National Laboratory, Reactor Engineering Division, 1954), by J. F. Mumm, U.S. Atomic Energy Commission, and Argonne National Laboratory (page images at HathiTrust)
• Pressure-temperature relation for constant-area compressible flow of a gas, considering heat transfer and friction with constant wall temperatures (Los Alamos Scientific Laboratory of the University of California, 1957), by Franklin P. Durham, U.S. Atomic Energy Commission, and Los Alamos Scientific Laboratory (page images at HathiTrust)
• Fast reactor rocket engines--heat transfer (Los Alamos Scientific Laboratory of the University of California, 1962), by Ralph S. Cooper, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• High thermal conductance devices utilizing the boiling of lithium or silver (Los Alamos Scientific Laboratory of the University of California, 1965), by John E. Deverall, J. E. Kemme, U.S. Atomic Energy Commission, and Los Alamos Scientific Laboratory (page images at HathiTrust)
• Satellite heat pipe (Los Alamos Scientific Laboratory of the University of California, 1965), by John E. Deverall, J. E. Kemme, U.S. Atomic Energy Commission, and Los Alamos Scientific Laboratory (page images at HathiTrust)
• Reactor Experimental Engineering Division. (Oak Ridge National Laboratory, 1952), by H. F. Poppendiek, L. D. Palmer, Oak Ridge National Laboratory, U.S. Atomic Energy Commission, and Carbide and Carbon Chemicals Corporation (page images at HathiTrust)
• Heat transfer in forced convection film boiling / LeRoy A. Bronley, Norman R. LeRoy and James A. Robbers. ([Lawrence] Radiation Laboratory, 1952), by LeRoy Alton Bromley, James A. Robbers, Norman R. LeRoy, Lawrence Radiation Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Effect of fluid properties on mass transfer in the gas phase ([Lawrence] Radiation Laboratory, 1953), by Edward Joseph Lynch, Charles R. Wilke, Lawrence Radiation Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heizungs-, Lüftungs- und Dampfkraftanlagen in den Vereinigten Staaten von Amerika. (R. Oldenburg, 1912), by Arthur K. Ohmes (page images at HathiTrust; US access only)
• Pressure and heat-transfer distribution on the afterbody of a lifting Mercury-type capsule at Mach number 15 in helium (National Aeronautics and Space Administration, 1963), by Joseph G. Marvin and Ames Research Center (page images at HathiTrust)
• Measurements of the surface flows, heat transfer, pressure distribution, and longitudinal stability of a mercury capsule model at Mach numbers of 6.9 and 9.6 (National Aeronautics and Space Administration, 1961), by Philip E. Everhart, Peter T. Bernot, and Langley Research Center (page images at HathiTrust)
• Heat-transfer and pressure measurements on a concove-nose cylinder for a mach number range of 2.49 to 4.44 (National Aeronautics and Space Administration, 1959), by Jr. Stallings, Paige B. Burbank, and Langley Research Center (page images at HathiTrust)
• Calculation of compressible turbulent boundary layers with pressure gradients and heat transfer (National Aeronautics and Space Administration ;, 1969), by Larry L. Lynes, Gary D. Kuhn, Jack Norman Nielsen, Nielsen Engineering & Research, and Ames Research Center (page images at HathiTrust)
• An integral analysis of heat transfer downstream of a rearward-facing step with small coolant injection. (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by Keiichi Karashima (page images at HathiTrust; US access only)
• Effect of chord size on weight and cooling characteristics of air-cooled turbine blades (National Advisory Committee for Aeronautics, 1957), by Jack B. Esgar, Arthur N. Curren, Eugene F. Schum, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Final report on studies in boiling heat transfer. (U.S. Atomic Energy Commission, Technical Information Service, 1951), by Los Angeles. Department of Engineering University of California, Llewellyn Michael Kraus Boelter, and U.S. Atomic Energy Commission. Chicago Operations Office (page images at HathiTrust)
• Heat transfer and pressure loss in proposed ORR fuel assemblies (United States Atomic Energy Commission, Technical Information Service ;, 1955), by J. P. Sanders, Oak Ridge National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Temperature coefficients and maximum rates of increase of reactivity for HRT (United States Atomic Energy Commission, Technical Information Extension ;, 1955), by V. K. Par©Øe, Oak Ridge National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Physical properties of UO₂SO₄-D₂O solutions and ThO₂-H₂O slurries (United States Atomic Energy Commission, Technical Information Service ;, 1955), by T. W. Leland, Oak Ridge National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heat removal systems for the HRT pressure vessel (United States Atomic Energy Commission, Technical Information Extension ;, 1956), by R. E. Aven, Oak Ridge National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heat removal from a proposed hydroclone underflow pot geometry for a volume heat source (Oak Ridge National Laboratory, 1955), by P. A. Haas, J. K. Langsdon, and U.S. Atomic Energy Commission (page images at HathiTrust)
• HRT space cooler heat load (Oak Ridge National Laboratory, 1955), by F. C. Zapp and U.S. Atomic Energy Commission (page images at HathiTrust)
• Effects of heat generation and heat removal on Homogeneous Reactor Test shutdown and dump (U.S. Atomic Energy Commission, Technical Information Service Extension, 1956), by M. W. Rosenthal, H. C. Claiborne, U.S. Atomic Energy Commission, and Oak Ridge National Laboratory (page images at HathiTrust)
• Status of liquid-metal-heated steam generator technology (Office of Technical Services, 1958), by Nyle A. Bischel, U.S. Atomic Energy Commission, and Babcock & Wilcox Company (page images at HathiTrust)
• Survey of methods for calculating gamma-ray heating (Oak Ridge National Laboratory, 1965), by H. C. Claiborne, Oak Ridge National Laboratory. Neutron Physics Division, Radiation Shielding Information Center (U.S.), Oak Ridge National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Experimental investigation of free-convection heat transfer in vertical tube at large grashof numbers (National Advisory Committee for Aeronautics, 1952), by E. R. G. Eckert, A. J. Diagula, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Experimental investigation of the heat-transfer characteristics of an air-cooled sintered porous turbine blade (National Advisory Committee for Aeronautics, 1952), by Louis J. Jr Schafer, Hadley T. Richards, Edward R. Bartoo, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Blade-to-coolant heat-transfer results and operating data from a natural-convection water-cooled single-stage turbine (National Advisory Committee for Aeronautics, 1951), by Anthony J. Diaguila, John C. Freche, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Determination of blade-to-coolant heat-transfer coefficients on a forced-convection, water-cooled, single-stage turbine (National Advisory Committee for Aeronautics, 1951), by John C. Freche, Eugene F. Schum, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Determination of gas-to-blade convection heat-transfer coefficients on a forced-convection, water-cooled single-stage aluminum turbine (National Advisory Committee for Aeronautics, 1951), by John C. Freche, Eugene F. Schum, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Correlation of heat-transfer and friction data for air flowing in inconel tube with rounded entrance (National Advisory Committee for Aeronautics, 1949), by Warren H. Lowdermilk, Milton D. Grele, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Heat transfer on an afterbody immersed in the separated wake of a hemisphere (National Advisory Committee for Aeronautics, 1958), by Helmer V. Nielsen, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
• Heat transfer to blunt nose shapes with laminar boundary layers at high supersonic speeds (National Advisory Committee for Aeronautics, 1957), by John O. Jr Reller, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
• Heat-transfer characteristics of blunt 2 and 3 dimensional bodies at supersonic speeds. (National Advisory Committee for Aeronautics, 1956), by Glen Goodwin, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
• Heat transfer from high-temperature surfaces to fluids. [Part] 1, Preliminary investigation with air in inconel tube with rounded entrance, inside diameter of 0.4 inch and length of 24 inches (National Advisory Committee for Aeronautics, 1948), by Leroy V. Humble, Milton Grele, Warren H. Lowdermilk, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
• A discussion of methods for reducing aerodynamic heating in supersonic flight (National Advisory Committee for Aeronautics, 1955), by A. J. Jr Eggers, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
• Heat transfer to lead-bismuth and mercury in laminar and transistor pipe flow (U.S. Atomic Energy Commission, Technical Information Service, 1953), by H. A. Johnson, W. J. Clabaugh, J. P. Hartnett, U.S. Atomic Energy Commission, and Berkeley. Institute of Engineering Research University of California (page images at HathiTrust)
• Effect of diameter of closed-end coolant passages on natural-convection water cooling of gas-turbine blades (National Advisory Committee for Aeronautics, 1956), by Arthur N. Curren, Charles F. Zalabak, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effect of blade-tip crossover passages on natural-convection water-cooling of gas-turbine blades (National Advisory Committee for Aeronautics, 1956), by Charles F. Zalabak, Arthur N. Curren, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Correlation of turbulent heat transfer in a tube for the dissociating system N204 <==> 2N02. (National Advisory Committee for Aeronautics, 1958), by Richard S. Brokaw, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Preliminary investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61 (National Advisory Committee for Aeronautics, 1952), by K. R. Czarnecki, Archibald R. Sinclair, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Experimental convective heat transfer to a 4-inch and 6-inch hemisphere at Mach numbers from 1.62 to 3.04 (National Advisory Committee for Aeronautics, 1954), by Leo T. Chauvin, Joseph P. Maloney, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration (National Advisory Committee for Aeronautics, 1955), by Charles B. Rumsey, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Local heat transfer to blunt noses at high supersonic speeds (National Advisory Committee for Aeronautics, 1957), by William E. Stoney, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Heat transfer and pressure measurement on a 5-inch hemispherical concave nose at a Mach number of 2.0 (National Advisory Committee for Aeronautics, 1958), by J. Thomas Markley, United States. National Adviosry Committee for Aeronautics, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Improved measurements of surface heat transfer by the method of cyclic temperature variations (U. S. Atomic Energy Commission, Technical Information Service, 1955), by C. E. Sealander, R. E. Grimble, S. L. Fawcett, Russell Wendt Dayton, Battelle Memorial Institute, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heat transfer from parallel rods in axial flow (Battelle Memorial Institute, 1955), by Sherwood L. Fawcett, Joel W. Chastain, Wayne B. Dell, David A. Dingee, U.S. Atomic Energy Commission, and Battelle Memorial Institute (page images at HathiTrust)
• Heat transfer and burnout to water at high subcritical pressures (Battelle Memorial Institute, 1956), by Harold M. Epstein, Sherwood L. Fawcett, Joel W. Chastain, U.S. Atomic Energy Commission, and Battelle Memorial Institute (page images at HathiTrust)
• Vapor formation and behavior in boiling heat transfer (Battelle Memorial Institute, 1957), by R. A. Egen, Joel W. Chastain, David A. Dingee, U.S. Atomic Energy Commission, Battelle Memorial Institute, and United States Navy Department Bureau of Ships (page images at HathiTrust)
• Boiling-water void distribution and slip ratio in heated channels : final report to Joint U.S.-Euratom Research and Development Board (Battelle Memorial Institute, 1961), by Joel W. Chastain, David A. Dingee, R. O. Wooton, Harold M. Epstein, Friedrich G. Peter, James J. Foglia, U.S. Atomic Energy Commission, and Battelle Memorial Institute (page images at HathiTrust)
• Analysis of turbulent free-convection boundary layer on flat plate (National Advisory Committee for Aeronautics, 1950), by E. R. G. Eckert, Thomas W. Jackson, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Analytical investigation of turbulent flow in smooth tubes with heat transfer with variable fluid properties for Prandtl number of 1 (National Advisory Committee for Aeronautics, 1950), by Robert G. Deissler and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Temperature distribution in internally heated walls of heat exchangers composed of noncircular flow passages (National Advisory Committee for Aeronautics, 1951), by E. R. G. Eckert, George M. Low, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Diffusion of heat from a line source in isotropic turbulence (National Advisory Committee for Aeronautics, 1952), by M. S. Uberoi, Stanley Corrsin, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Analysis of turbulent heat transfer, mass transfer, and friction in smooth tubes at high Prandtl and Schmidt numbers (National Advisory Committee for Aeronautics, 1954), by Robert G. Deissler and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Exact solutions of laminar-boundary-layer equations with constant property values for porous wall with variable temperature (National Advisory Committee for Aeronautics, 1954), by Patrick L. Donoughe, John N. B. Livingood, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Approximate calculation of the temperature distribution surrounding coolant holes in a heat generating solid with finite value of fluid heat transfer coefficient (Los Alamos Scientific Laboratory of the University of California, 1960), by T. R. Regenie, J. C. Rowley, U.S. Atomic Energy Commission, and Los Alamos Scientific Laboratory (page images at HathiTrust)
• Oxygen-oil explosions. Preliminary report I, General outline of the problem and summary of results to date (U.S. Dept. of the Interior, Bureau of Mines, 1923), by Mayo Dyer Hersey and United States Bureau of Mines (page images at HathiTrust)
• Heat capacity and magnetic susceptibility of thulium ethylsulfate (Ames Laboratory, Iowa State University of Science and Technology, 1960), by B. C. Gerstein, F. H. Spedding, Ames Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Large Bridgman type unit for preparing large and small diameter single crystals (Ames Laboratory, 1962), by Robert E. Slonaker, Edwin H. Olson, Morton Smutz, U.S. Atomic Energy Commission, and Ames Laboratory (page images at HathiTrust)
• Determination of turbulent thermal diffusivities for flow of liquids in pipes (Ames Laboratory, Iowa State University of Science and Technology, 1963), by William F. Beckwith, Ray Fahien, Ames Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Temperature distribution in a hollow cylindrical manometer column (Ames Laboratory, Iowa State University of Science and Technology, 1963), by Dale LeRoy Smith, Ray W. Fisher, Ames Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Peak heat flux in nucleate boiling heat transfer (Ames Laboratory, Iowa State University of Science and Technology, 1964), by Bernard Patrick Breen, George Burnet, Ames Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Thermal stress analysis of a cylinder of semi-plastic material (United States Atomic Energy Commission, Technical Information Service, 1956), by Donald Hunter, Glenn Murphy, Ames Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Analysis of turbulent heat transfer and flow in the entrance regions of smooth passages (National Advisory Committee for Aeronautics, 1953), by Robert G. Diessler, Lewis Research Center, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Conditioning and steady-state performance of SNAP-8 tube-in-shell mercury boiler (National Aeronautics and Space Administration ;, 1967), by James A. Albers, Sol H. Gorland, William T. Wintucky, and Lewis Research Center (page images at HathiTrust)
• Apollo fuel-cell condenser heat-transfer tests (National Aeronautics and Space Administration ;, 1966), by Michael B. Weinstein and Lewis Research Center (page images at HathiTrust)
• Experimental feasibility study of water-filled capillary-pumped heat-transfer loops (National Aeronautics and Space Administration ;, 1966), by Francis J. Stenger and Lewis Research Center (page images at HathiTrust)
• Heat-transfer and pressure measurements of a 1/7-scale model of a Mercury capsule at angles of attack from 0° to ±20° at mach numbers of 3.50 and 4.44 (National Aeronautics and Space Administration, 1961), by Nancy L. Taylor, Paige B. Burbank, Ward F. Hodge, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Heat transfer to blunt axially symmetric bodies (National Aeronautics and Space Administration, 1960), by John O. Reller and Ames Research Center (page images at HathiTrust; US access only)
• Experimental data on stagnation-point gas injection cooling on a hemisphere-cone in a hypersonic arc tunnel (National Aeronautics and Space Administration ;, 1964), by John E. Grimaud, Leonard C. McRee, and Langley Research Center (page images at HathiTrust)
• Gas-suspension coolant project, final report (Office of Technical Information Extension, 1959), by U.S. Atomic Energy Commission and Babcock & Wilcox Company. Atomic Energy Division (page images at HathiTrust; US access only)
• Mixer-settler development : use of a shrouded paddle (E.I. du Pont de Nemours & Co., Explosives Dept., Atomic Energy Division, Technical Division, Savannah River Laboratory, 1955), by William J. Mottel, E. J. Weber, G. S. Nichols, U.S. Atomic Energy Commission, Savannah River Laboratory, and E.I. du Pont de Nemours & Company (page images at HathiTrust; US access only)
• Heat and mass transfer in a turbine contactor (E.I. du Pont de Nemours & Company, Savannah River Laboratory, 1963), by Donald S. Webster, U.S. Atomic Energy Commission, Savannah River Laboratory, and E.I. du Pont de Nemours & Company (page images at HathiTrust)
• Heat transfer burnout of a surface contacted by a spacer rib (E.I. du Pont de Nemours & Co., Explosives Dept., Atomic Energy Division, Technical Division, Savannah River Laboratory, 1961), by Samuel Mirshak, N. Dinos, R. H. Towell, U.S. Atomic Energy Commission, Savannah River Laboratory, and E.I. du Pont de Nemours & Company (page images at HathiTrust)
• Mixing efficiency in mixer-settlers : the effect of flow and paddle variables (E.I. du Pont de Nemours & Co., Explosives Dept., Atomic Energy Division, Technical Division, Savannah River Laboratory, 1957), by William J. Mottel, Thomas J. Colven, U.S. Atomic Energy Commission, Savannah River Laboratory, and E.I. du Pont de Nemours & Company (page images at HathiTrust)
• Turbine contactor for solvent extraction (E.I. du Pont de Nemours & Co., Explosives Dept., Atomic Energy Division, Technical Division, Savannah River Laboratory, 1958), by G. Starr Nichols, U.S. Atomic Energy Commission, Savannah River Laboratory, and E.I. du Pont de Nemours & Company (page images at HathiTrust)
• Heat transfer conditions during severe nuclear excursions in water cooled reactors (USAEC, Technical Information Service ;, 1959), by K. Hikido, U.S. Atomic Energy Commission, and General Electric Company (page images at HathiTrust)
• Two-phase pressure drop, burnout, and hydraulic oscillation of an inclined test section with net steam generation at 1000 PSIA (United States Atomic Energy Commission, Office of Technical Information, 1959), by S. Levy, C. L. Swan, General Electric Company. Atomic Power Equipment Department, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Superheat process tube heat transfer tests nuclear superheat project (General Electric Company, 1960), by E. Janssen, U.S. Atomic Energy Commission, and General Electric Company (page images at HathiTrust)
• Preliminary results from a free-flight investigation of boundary-layer transition and heat transfer on a highly polished 8-inch-diameter hemisphere-cylinder at Mach numbers up to 3 and Reynolds numbers based on a length of 1 foot up to 17.7 x 10⁶ (National Advisory Committee for Aeronautics, 1957), by J. R. Hall, Robert O. Piland, Katherine C. Speegle, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Heat transfer to bodies at angles of attack (National Advisory Committee for Aeronautics, 1957), by William V. Feller, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Heat-transfer measurements in free flight at Mach numbers up to 14.6 on a flat-faced conical nose with a total angle of 29° (National Advisory Committee for Aeronautics, 1958), by Charles B. Rumsey, Dorothy B. Lee, United States. National Adviosry Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• The transformation of heat in an engine (National Advisory Committee for Aeronautics ;, 1929), by Kurt Neumann and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• APEX-391 (General Electric, Atomic Products Division, Aircraft Nuclear Propulsion Dept., 1958), by J. F. Heyda and General Electric Company. Aircraft Nuclear Propulsion Department (page images at HathiTrust)
• Steady-state and transient thermal stresses in a tube subjected to internal heating (General Electric, Aircraft Nuclear Propulsion Dept., Atomic Products Division, 1959), by H.A. Eagle, A.L. Ross, and General Electric Company. Aircraft Nuclear Propulsion Department. Atomic Products Division (page images at HathiTrust)
• Steady-state and transient thermal stresses in a tube subjected to internal heating (General Electric, Aircraft Nuclear Propulsion Dept., Atomic Products Division, 1959), by H.A. Eagle, A.L. Ross, and General Electric Company. Aircraft Nuclear Propulsion Department. Atomic Products Division (page images at HathiTrust)
• Thermal stresses in tube with axial temperature gradient (General Electric, Aircraft Nuclear Propulsion Dept., Atomic Products Division, 1959), by R. J. Dunholter and General Electric Company. Aircraft Nuclear Propulsion Department. Atomic Products Division (page images at HathiTrust)
• Design and operation of a sodium-to-lithium-to air heat transfer system (General Electric, Technical Publications Subsections, 1957), by A. R. Crocker and General Electric Company. Aircraft Nuclear Propulsion Department. Atomic Products Division (page images at HathiTrust; US access only)
• Multigroup, multiregion, one-space-dimension photon-diffusion theory calculation - program FN-gamma : (ANP program no.728) (General Electric, Aircraft Nuclear Propulsion Dept., 1961), by M.S. Ferry, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heated annuli computer program (General Electric, Nuclear Materials and Propulsion Operation., 1961), by N. Clark, R. R. Jordan, R. N. Noyes, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heat transmission by radiation, conduction and convection (D. Van Nostrand company ..., 1921), by R. Royds (page images at HathiTrust)
• Heat transmission tables. (Heating and Ventilating Magazine Co., 1919), by William Russell Jones (page images at HathiTrust)
• O vni︠e︡shneĭ teploprovodnosti serebri︠a︡nykh provolok v vodi︠e︡ (Tip. V. Demakova, 1903), by E. Rogovskīĭ (page images at HathiTrust; US access only)
• Thermal warping of graphite pile (U.S. Atomic Energy Commission, Technical Information Service ;, 1943), by S. G. Bankoff, G. Rosner, C. P. Cabell, United States. Office of Scientific Research and Development. Metallurgical Laboratory, and U.S. Atomic Energy Commission. Technical Information Service (page images at HathiTrust)
• Heat transfer and pressure drop in a vertical square tube (Goodyear Atomic Corporation ;, 1958), by H. L. Foltz, Goodyear Atomic Corporation, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Free convection in narrow vertical liquid metal annuli (U.S. Atomic Energy Commission, Technical Information Service Extension ;, 1955), by D. P. Timo, Knolls Atomic Power Laboratory, and U.S. Atomic Energy Commission. Technical Information Service (page images at HathiTrust)
• Theory and application of sliding contact of metals in sodium (United States Atomic Energy Commission, Technical Information Service ;, 1955), by L. F. Coffin, Knolls Atomic Power Laboratory, U.S. Atomic Energy Commission, and General Electric Company (page images at HathiTrust)
• The effect of air injection on the heat transfer from a flat plate (1956), by Hugh Won Chan (page images at HathiTrust; US access only)
• Determination of burnout limits of polyphenyl coolants (Liquid Engine Division, Aerojet-General Corporation, 1958), by K. Sato, U.S. Atomic Energy Commission. Civilian Power Reactors Branch, and Aerojet-General Corporation. Liquid Engine Division (page images at HathiTrust)
• Graphical solutions of the non-boiling and surface boiling heat transfer equations (Livermore Research Laboratory of the U.S. Atomic Energy Commission operated by California Research & Development Co., 1953), by D. F. Casey, U.S. Atomic Energy Commission, Lawrence Livermore Laboratory, and California Research and Development Company (page images at HathiTrust)
• Advanced organic moderated reactor coolant screening and boiling test loops (Atomics International, 1960), by J. E. Leary, D. A. Huber, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Piqua organic moderated reactor purification system development (Atomics International, 1960), by W. N. Bley, R. W. Burkhardt, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heat transfer measurements in connection with thermal insulation of low-cost housing. (U.S. Dept. of Commerce, National Bureau of Standards, 1938), by United States. National Bureau of Standards (page images at HathiTrust)
• Reactor design and evaluation progress report... (North American Aviation, Inc. ;, 1953), by U.S. Atomic Energy Commission. Technical Information Center and North American Aviation. Atomics International Division (page images at HathiTrust)
• Heat transfer by natural convection from horizontal cylinders to liquid metals final report for July 1, 1949 to June 30, 1950. (Oak Ridge, Tennessee : United States Atomic Energy Commission, Technical Information Service, 1950., 1950), by Seymour C. Hyman, Charles F. Bonilla, Columbia University, and U.S. Atomic Energy Commission. New York Operations Office (page images at HathiTrust)
• Temperature distribution in a hollow cylindrical cup with a stem (Atomics International, 1962), by Guy W. Lehman, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Pool boiling investigation of benzene, diphenyl, and benzene-diphenyl mixtures under pressure (Atomics International, 1961), by D. A. Huber, J. C. Hoehne, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• An experimental study of sodium pool boiling heat transfer (Atomics International, 1962), by R. C. Noyes, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• An up-to-date review of the principles of heat transfer, with particular application to nuclear power (Gibbs and Cox, Inc., 1949), by Charles F. Bonilla and U.S. Atomic Energy Commission (page images at HathiTrust)
• Moderator graphite experiments in the Sodium Reactor Experiment (1958), by R. E. Taylor, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Forced convection heat transfer characteristics of polyphenyl reactor coolants (Atomics International, 1959), by M. Silberberg, D. A. Huber, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Stress-strain-temperature-time relationships for refractory materials (Atomics International, 1958), by R. D. Chipman, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Study of real gas and heat transfer effects on the design of hotshot wind tunnels (Sandia Corporation, Technical Information Division ;, 1960), by Jackson R. Stalder, David K. Eberly, Morris W. Rubesin, Inc Vidya, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
• Heat transfer across annuli in gas bonded uranium dioxide fuel elements (Atomics International, 1960), by J. W. Carroll, C. A. Smith, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Digital code for transient two-phase flow and heat transfer (Atomics International, 1965), by R. C. Noyes, H. H. Cappel, J. G. Morgan, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heat transfer and pressure drop in eccentric annuli (Oak Ridge, Tennessee : United States Atomic Energy Commission, Technical Information Service, 1961., 1961), by Theodore Diskind, U.S. Atomic Energy Commission. New York Operations Office, and Columbia University (page images at HathiTrust)
• The frequency response of nucleate pool boiling heat transfer (Oak Ridge, Tennessee : United States Atomic Energy Commission, Technical Information Service, 1964., 1964), by Robert C. Lummis, Columbia University. Engineering Research Laboratories, and U.S. Atomic Energy Commission. New York Operations Office (page images at HathiTrust)
• Comparative effectiveness of a convection-type and a radiation-type cooling cap on a turbosupercharger (National Advisory Committee for Aeronautics ;, 1946), by Frederick J. Hartwig and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Preliminary heat transfer studies of organic moderated reactor fuel elements (Atomics International, 1957), by E. B. Baumeister, C. W. Wheelock, U.S. Atomic Energy Commission. Technical Information Center, and North American Aviation. Atomics International Division (page images at HathiTrust)
• Calculation of surface temperatures in steady supersonic flight (National Advisory Committee for Aeronautics ;, 1946), by George P. Wood and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Note of similarity conditions for flows with heat transfer (National Advisory Committee for Aeronautics, 1948), by Albert E. Von Doenhoff and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Heat flow in the trigger of a reactor safety device (Atomics International, 1958), by Thomas H. Springer, Norman C. Miller, U.S. Atomic Energy Commission. Technical Information Center, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Boiling burnout progress (Washington, D.C. : Department of Commerce, Office of Technical Services, 1955-., in the 20th century), by John E. Viscardi, U.S. Atomic Energy Commission, and Nuclear Development Corporation of America (page images at HathiTrust)
• Reactor heat transfer progress (Washington, D.C. : Department of Commerce, Office of Technical Services., 1956), by John E. Viscardi, U.S. Atomic Energy Commission, and Nuclear Development Corporation of America (page images at HathiTrust)
• Further experiments on the flow and heat transfer in a heated turbulent air jet (National Advisory Committee for Aeronautics, 1949), by Stanley Corrsin, M. S. Uberoi, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• The Effect of an arbitrary surface-temperature variation along a flat plate on the convective heat transfer in an incompressible turbulent boundary layer (National Advisory Committee for Aeronautics, 1951), by Morris W. Rubesin and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Heat, mass, and momentum transfer for flow over a flat plate with blowing or suction (National Advisory Committee for Aeronautics, 1954), by H. S. Mickley and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), by Benjamin Pinkel, Everett Bernardo, Eugene J. Manganiello, Aircraft Engine Research Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Single tube heat transfer and pressure drop tests (United States Atomic Energy Commission, Office of Technical Information ;, 1961), by S. Frank, M. Norin, J. Jicha, U.S. Atomic Energy Commission, and Martin Company. Nuclear Division (page images at HathiTrust)
• Local boiling heat transfer tests (United States Atomic Energy Commission, Division of Technical Information ;, 1961), by J. J. Jicha, S. Frank, Martin Company. Nuclear Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Investigation of tetralin explosion (Atomics International, 1960), by J. S. McDonald, J. S. Owens, J. E. Owens, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Development of ferritic steels for high temperature sodium service. Part I, 2.25 CR - 1 Mo - 0.4 Cb - 0.4 Ti experimental alloy (Atomics International, 1960), by W. C. Hayes, A. J. Birkle, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Pressure loss and heat transfer for turbulent flow. (U. S. Atomic Energy Commission, Office of Technical Information, 1960), by Rudolph Koch (page images at HathiTrust)
• Boiling water reactor technology status of the art report / [edited by C. Victor Pearson]. (Reactor Engineering Division, Argonne National Laboratory, 1962), by C. Victor Pearson and Argonne National Laboratory. Reactor Engineering Division (page images at HathiTrust)
• Effect of wetting on heat transfer characteristics of liquid metals : (thesis) / W. K. Stromquist. (Oak Ridge, Tennessee : United States Atomic Energy Commission, Technical Information Service, 1953., 1953), by W. K. Stromquist and U.S. Atomic Energy Commission (page images at HathiTrust)
• Effect of gas entrainment on the heat transfer characteristics of mercury under turbulent flow conditions : final report (Oak Ridge, Tennessee : United States Atomic Energy Commission, Technical Information Service, 1955., 1955), by Harold Chelemer and U.S. Atomic Energy Commission. Technical Information Service (page images at HathiTrust)
• Investigation of materials for use in a heat transfer system containing liquid lead alloys, report no. XII : final report April 1, 1950 to June 30, 1951 (Oak Ridge, Tennessee : United States Atomic Energy Commission, Technical Information Service, 1955., 1955), by Ralph Parkman, O. Cutler Shepard, and U.S. Atomic Energy Commission. Technical Information Service (page images at HathiTrust)
• Evaluation and performance of once-through, zero-gravity boiler tubes with two-phase water (Middletown, Connecticut : Pratt & Whitney Aircraft Division, United Aircraft Corporation, CANEL Operations ; Washington, D.C. : Available from the Office of Technical Services, 1964., 1964), by E. Bernstein, J. Meregian, J. P. Petrek, U.S. Atomic Energy Commission, and United Aircraft Corporation. Pratt & Whitney Aircraft Division (page images at HathiTrust)
• Experimental results of forced convection boiling potassium heat transfer and pressure drop tests (Middletown, Connecticut : Pratt & Whitney Aircraft Division, United Aircraft Corporation, CANEL Operations ; Washington, D.C. : Available from the Office of Technical Services, 1964., 1964), by E. Bernstein, J.J. Horan, G.J. Rose, J.P. Petrek, U.S. Atomic Energy Commission, and United Aircraft Corporation. Pratt & Whitney Aircraft Division (page images at HathiTrust)
• Study of plutonium oxide heat generation in a wood moderated container (Denver, Colorado : Dow Chemical Company, Rocky Flats Plant ; Washington, D.C : Office of Technical Services, Department of Commerce, 1964., 1964), by J. D. Moseley, U.S. Atomic Energy Commission, and Dow Chemical Company. Rocky Flats Division (page images at HathiTrust)
• Temperature variation, heat transfer, and void volume development in the transient atmospheric boiling of water (Springfield, Virginia : U.S. Department of Commerce, National Technical Information Service, 1961., 1961), by H. A. Johnson, Z. R. Rosztoczy, J.H. Lienhard, F.B. Selph, V. E. Schrock, U.S. Atomic Energy Commission. Division of Reactor Development, United States. Department of Energy. San Francisco Operations Office, and Berkeley. Institute of Engineering Research University of California (page images at HathiTrust)
• Heat transfer : a bibliography of unclassified report literature (Oak Ridge, Tennessee : U.S. Atomic Energy Commission, Technical Information Service Extension, 1957., 1957), by James M. Jacobs, Gifford A. Young, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Basic studies in heat transfer and fluid flow. (New York, New York : Columbia University, Dept. of Chemical Engineering, Engineering Research Laboratories., in the 1950s), by U.S. Atomic Energy Commission. Office of Technical Information and Columbia University. Engineering Research Laboratories (page images at HathiTrust)
• Transmission of heat through building materials (Minneapolis, 1923), by Frank Benjamin Rowley (page images at HathiTrust)
• Reactor heat transfer conference of 1956; collected papers and reports of a conference held at New York, November 1 and 2, 1956. (Oak Ridge, Tennessee : United States Atomic Energy Commission, Technical Information Service Extension, 1957., 1957), by U.S. Atomic Energy Commission, John E. Viscardi, and Nuclear Development Corporation of America (page images at HathiTrust)
• Thermophysical and transport properties of high temperature energy storage materials (Oak Ridge, Tennessee : United States Atomic Energy Commission, Technical Information Service Extension, 1964., 1964), by R. A. Sharma, H. Chang, U.S. Atomic Energy Commission, and University of Pennsylvania (page images at HathiTrust)
• Heat transfer and pressure drop for a gas at high temperature : technical report 247-2 (Oak Ridge, Tennessee : United States Atomic Energy Commission, Technical Information Service Extension, 1961., 1961), by Monty E. Davenport, George Leppert, Patrick Magee, Stanford University. Department of Mechanical Engineering, and U.S. Atomic Energy Commission (page images at HathiTrust)
• The effect of transverse temperature gradients on the heat transfer and friction for laminar flow of gases : technical report no. 247-3 (Oak Ridge, Tennessee : United States Atomic Energy Commission, Technical Information Service Extension, 1962., 1962), by Monty E. Davenport and U.S. Atomic Energy Commission. Division of Technical Information (page images at HathiTrust)
• The carbon arc image furnace (Washington, D.C. : Office of Technical Services, Department of Commerce, 1956., 1956), by T. P. Davis, University of Rochester. Atomic Energy Project, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Investigation of burnout heat flux in rectangular channels at 2000 psia (Oak Ridge, Tennessee : U.S. Atomic Energy Commission, Technical Information Service Extension, 1955., 1955), by H. S. Jacket, J. E. Zerbe, J. D. Roarty, Westinghouse Electric Corporation, Bettis Atomic Power Laboratory, and U.S. Atomic Energy Commission. Technical Information Service Extension (page images at HathiTrust)
• Pressure drop in two-phase flow (Argonne National Laboratory, Reactor Engineering Division, 1952), by D. H. Weiss and Argonne National Laboratory (page images at HathiTrust)
• CVR pressurizer simulator study (Washington, D.C. : Office of Technical Services, Department of Commerce, 1953., 1953), by W. M. Gajewski, J. N. Grace, Bettis Atomic Power Laboratory, U.S. Atomic Energy Commission, and Westinghouse Electric Corporation. Atomic Power Department (page images at HathiTrust)
• PWR plant container sizing criteria : studies of transient temperature and pressure in plant container following primary coolant system rupture (Washington, D.C. : Office of Technical Services, Department of Commerce, 1957., 1957), by R. M. Rome, T. R. Moffette, Westinghouse Electric Corporation, U.S. Atomic Energy Commission, and Bettis Atomic Power Laboratory (page images at HathiTrust)
• Investigation of a seeded PWR (Washington, D.C. : Office of Technical Services, Department of Commerce, 1955., 1955), by Bettis Atomic Power Laboratory, Westinghouse Electric Corporation. Atomic Power Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Two-phase heat transfer, Bibliography on (Washington, D.C. : Office of Technical Services, Department of Commerce, 1960., 1960), by G. W. Maurer, Westinghouse Electric Corporation, U.S. Atomic Energy Commission, and Bettis Atomic Power Laboratory (page images at HathiTrust)
• Analysis of check valve disc motion during a flow transient (Washington, D.C. : Office of Technical Services, Department of Commerce, 1962., 1962), by G. M. Fuls, Bettis Atomic Power Laboratory, Westinghouse Electric Corporation, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Report of the director. Heat transmission through building materials (J.L.L. Kuhn, printer to the Commonwealth, 1917), by James Ambrose Moyer (page images at HathiTrust)
• Design basis for critical heat flux condition in boiling water reactors (San Jose, California : General Electric Company, Atomic Power Equipment Department, 1966., 1966), by J. M. Healzer, S. Levy, E. Janssen, J. E. Hench, U.S. Atomic Energy Commission, and General Electric Company. Atomic Power Equipment Department (page images at HathiTrust)
• Heat transfer measurements at sodium - stainless steel interface (Schenectady, New York : Knolls Atomic Power Laboratory, 1951., 1951), by James W. Moyer, W. A. Riemen, Knolls Atomic Power Laboratory, General Electric Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Analysis of the unsteady state in the thermal diffusion cell (Miamisburg, Ohio : Mound Laboratory, 1963., 1963), by Tokur©Æo Mizushina, Ryusho Ito, Monsanto Chemical Company, Monsanto Research Corporation, Mound Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Gas cooling of a porous heat source (Downey, California : Atomic Energy Research Department, North American Aviation, Inc., 1951, 1951), by L. Green, B. J. Lemke, U.S. Atomic Energy Commission, and North American Aviation (page images at HathiTrust)
• Proceedings, September 28-29, 1965. (USAEC Division of Technical Information Extension], 1965), by Ill.) Conference on Application of High Temperature Instrumentation to Liquid-Metal Experiments (1965 : Argonne, Ruth N. Weltmann, R. M. Scroggins, Paul Albert Lottes, University of Chicago, United States National Aeronautics and Space Administration, U.S. Atomic Energy Commission, and Argonne National Laboratory (page images at HathiTrust)
• Heat transfer in condensation and boiling (Teploperedacha pri Kondensatsii i Kipenii) (U. S. Atomic Energy Commission, Technical Information Service, 1959), by S. S. Kutateladze (page images at HathiTrust)
• Workshop on Heat and Mass Transfer in Porous Media : held at Case Western Reserve University, Cleveland, Ohio, Oct. 14-15, 1974 (Case Western Reserve University?, 1975), by Workshop on Heat and Mass Transfer in Porous Media (1974 : Case Western Reserve University), A. Dybbs, National Science Foundation (U.S.), and Thermal and Aerospace Sciences Case Western Reserve University. Department of Fluid (page images at HathiTrust; US access only)
• Applied thermodynamics and heat transfer (Foreign Technology Division, Air Force Systems Command], 1963), by I. I. Novikov and Kirill Dmitrievich Voskresenskiĭ (page images at HathiTrust)
• Collection of heat-transfer properties of gases at moderate pressures, and rules for rapid estimation of missing data (Schenectady, N. Y., 1962), by Franz Josef Neugebauer, United States. Office of Naval Research. Material Sciences Division, and General Electric Company. General Engineering Laboratory (page images at HathiTrust; US access only)
• Liquid metals : Collection of articles. (Selected articles) (U.S. Atomic Energy Commission, 1965), by V. M. Borishanskiĭ (page images at HathiTrust; US access only)
• ...Heat transfer in a commercial heat exchanger (The University, 1931), by Byron Elliott Short and M. Mendell Heller (page images at HathiTrust; US access only)
• Observations of flow characteristics of volume-heated boiling pools (Upton, New York : Brookhaven National Laboratory, Department of Nuclear Energy, Experimental Modeling Group, 1977., 1977), by T. Ginsberg, J. C. Chen, C. E. Schwarz, Owen C. Jones, and Brookhaven National Laboratory. Department of Nuclear Energy. Experimental Modeling Group (page images at HathiTrust)
• Heat transfer and fluid dynamic characteristics of internally heated boiling pools (Upton, New York : Brookhaven National Laboratory, Department of Applied Science, Reactor Safety Experiments Group, 1977., 1977), by W. R. Gustavson, Mujid S. Kazimi, J. C. Chen, and Brookhaven National Laboratory. Department of Applied Science (page images at HathiTrust)
• Thermo-fluid mechanics of volume-heated boiling pools (Upton, New York : Brookhaven National Laboratory, Department of Nuclear Energy, 1977., 1977), by G. Alanson Greene, C. E. Schwarz, Owen C. Jones, Brookhaven National Laboratory. Thermal Hydraulic Development Division, and U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research (page images at HathiTrust)
• Heat transfer considerations in the temperature control of instrumentation packages at high altitudes (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1965., 1965), by Arnold Piacentini, Darrel E. Dube, Kenneth H. Lindenfelser, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Interaction of a buoyant turbulent round jet with a co-flowing wind (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1975), by Milton M. Klein, Bruce A. Kunkel, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Heat transfer with continuous and discrete heating in fully developed turbulent channel flow : an application to convective cooling of a nuclear waste repository drife (Office of Nuclear Waste Isolation, Battelle Memorial Institute, 1981), by D. W. Gear, F. A. Kulacki, R. N. Christensen, United States. Department of Energy, and Battelle Memorial Institute. Office of Nuclear Waste Isolation (page images at HathiTrust)
• Heat transfer and pressure drop for air flowing in small tubes (Oak Ridge, Tennessee : Fairchild Engine and Airplane Corporation, 1950., 1950), by William H. McAdams, C. L. Kroll, J. N. Addoms, Fairchild Engine and Airplane Corporation, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Experimental forced-convection heat transfer with adiabatic walls and internal heat generation in a liquid metal (Oak Ridge, Tennessee : Oak Ridge National Laboratory, [1959], 1959), by G. L. Muller, Oak Ridge National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Effect of wetting on heat transfer characteristics of liquid metals : second quarterly report (Oak Ridge, Tennessee : U.S. Atomic Energy Commission, Technical Information Service, 1951., 1951), by W. K. Stromquist, Robert Marsh Boarts, Knoxville University of Tennessee, and U.S. Atomic Energy Commission. Technical Information Service (page images at HathiTrust)
• Effect of wetting on heat transfer characteristics of liquid metals : fourth quarterly report (Oak Ridge, Tennessee : U.S. Atomic Energy Commission, Technical Information Service, 1952., 1952), by Robert Marsh Boarts, W. K. Stromquist, Knoxville University of Tennessee, and U.S. Atomic Energy Commission. Technical Information Service (page images at HathiTrust)
• Effect of wetting on heat transfer characteristics of liquid metals : quarterly report for period May 1 - July 31, 1952 (Oak Ridge, Tennessee : U.S. Atomic Energy Commission, Technical Information Service, 1952., 1952), by Robert Marsh Boarts, W. K. Stromquist, H. Chelemer, Knoxville University of Tennessee, U.S. Atomic Energy Commission, and U.S. Atomic Energy Commission. Technical Information Service (page images at HathiTrust)
• Effect of wetting on heat transfer characteristics of liquid metals : progress report (Oak Ridge, Tennessee : U.S. Atomic Energy Commission, Technical Information Service, 1953., 1953), by Robert Marsh Boarts, Bernard Hoffman, Harold Chelemer, Knoxville University of Tennessee, and U.S. Atomic Energy Commission. Technical Information Service (page images at HathiTrust)
• Effect of wetting on heat transfer characteristics of liquid metals : a progress report (Oak Ridge, Tennessee : U.S. Atomic Energy Commission, Technical Information Service, 1954., 1954), by Robert Marsh Boarts, Bernard Hoffman, Harold Chelemer, Knoxville University of Tennessee, and U.S. Atomic Energy Commission. Technical Information Service (page images at HathiTrust)
• Flow of fluids through valves, fittings, and pipe. (Crane Co., 1957), by Crane Company. Engineering Division (page images at HathiTrust; US access only)
• Study of heat transfer and fouling of heat transfer surfaces in the deep ocean : final report (C.F. Braun & Co., 1965), by C.F. Braun & Co (page images at HathiTrust)
• Inquiry in relation to the alleged influence of colour on the radiation of non-luminous heat ([Franklin Institute?], 1835), by A. D. Bache (page images at HathiTrust)
• Effect of wetting on heat transfer characteristics of liquid metals : third quarterly report (Oak Ridge, Tennessee : U.S. Atomic Energy Commission, Technical Information Service, 1952., 1952), by W. K. Stromquist, R. M. Boarts, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heat transfer to water in turbulent flow in internally heated annuli (New York, New York : Columbia University, Department of Chemical Engineering, 1955., 1955), by Ralph P. Stein, William Begell, Columbia University. Department of Chemical Engineering, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heat transfer rates to boiling freon 114 in vertical tubes (Portsmouth, Ohio : Goodyear Atomic Corporation, 1958., 1958), by H. L. Foltz, U.S. Atomic Energy Commission, and Goodyear Atomic Corporation (page images at HathiTrust)
• Minnesota 1973 atmospheric boundary layer experiment data report (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1976), by Yutaka Izumi, James S. Caughey, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Gas replenishment techniques for use in high-altitude, long-duration scientific balloon flights (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1979., 1979), by Andrew S. Carten, Charles F. Sindt, and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• Double Fourier series solution of Poisson's equation on a sphere (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1980., 1980), by Samuel Y. K. Yee and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• Advective heating in the thermosphere during geomagnetic storms (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1972., 1972), by J. M. Forbes and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• A mathematical model of the evolution of radiation fog (L.G. Hanscom FIeld, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1972., 1972), by I. M. Zakharova and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Numerical experiments in forecasting air and soil temperature profiles (Bedford, Massachusetts : Atmospheric Circulations Laboratory, Geophysics Research Directorate, Air Force Cambridge Research Center, 1959., 1959), by Donald W. Stevens and Air Force Cambridge Research Center (U.S.). Geophysics Research Directorate (page images at HathiTrust)
• Comparisons of experimental and theoretical heat transfer to a yawed sphere-cone model at supersonic speeds (White Oak, Maryland : United States Naval Ordnance Laboratory, 1964., 1964), by Lionel Pasiuk and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Skin friction and heat transfer characteristics of the compressible laminar boundary layer with injection of a light, medium, and heavy gas (White Oak, Maryland : United States Naval Ordnance Laboratory, 1967., 1967), by L. M. Albacete, W. J. Glowacki, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• An approximate method for the calculation of the reynolds analogy factor for a compressible turbulent boundary layer in a pressure gradient (White Oak, Maryland : United States Naval Ordnance Laboratory, 1967., 1967), by Neal Tetervin and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• A correlation of heat-transfer and skin-friction data and an experimental Reynolds analogy factor for highly cooled turbulent boundary layers at Mach 5.0 (White Oak, Maryland : United States Naval Ordnance Laboratory, 1969., 1969), by Donald M. Wilson and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Balance for measuring skin friction in the presence of heat transfer (White Oak, Maryland : United States Naval Ordnance Laboratory, 1969., 1969), by James R. Bruno, Donald B. Risher, William Joseph Yanta, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Velocity profile, skin-friction balance and heat-transfer measurements of the turbulent boundary layers at Mach 5 and zero-pressure gradient (White Oak, Maryland : United States Naval Ordnance Laboratory, 1969., 1969), by Roland E. Lee, A. C. Leonas, William Joseph Yanta, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• The prediction of errors and the improvement of data obtained in wind-tunnel heat-transfer tests (White Oak, Maryland : United States Naval Ordnance Laboratory, 1970., 1970), by Donald M. Wilson and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Measurements of a mach 4.9 zero-pressure-gradient turbulent boundary layer with heat yransfer. Part 1, Data compilation (White Oak, Maryland : United States Naval Ordnance Laboratory, 1972., 1972), by Robert L. P. Voisinet, Roland E. Lee, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Hypersonic, turbulent, cold-wall, skin-friction and heat-transfer measurements on an axisymmetric sharp cone (White Oak, Maryland : United States Naval Ordnance Laboratory, 1973., 1973), by Kuei-Yuan Chien, Md.) Naval Ordnance Laboratory (White Oak, and Technical Cooperation Program (page images at HathiTrust)
• The performance of finned-circular-tube heat exchanger surfaces (Stanford, California, Department of Mechanical Engineering, Stanford University, 1951., 1951), by D. W. Johnson (page images at HathiTrust)
• Numerical differentiation by spline functions and its application to analyzing a lake temperature observation (Corps of Engineers, U.S. Army, Cold Regions Research and Engineering Laboratory, 1971), by Shunsuke Takagi and Cold Regions Research and Engineering Laboratory (U.S.) (page images at HathiTrust)
• A numerical study of the velocity and temperature fields in a stratified reservoir with artificial thermal inputs (Energy Systems Laboratories, Center for Research in Water Resources, University of Texas at Austin, 1974), by Larry I. Crow and W. L. Oberkampf (page images at HathiTrust; US access only)
• Heat transfer analysis for unsteady high velocity pipe flow (Iowa Institute of Hydraulic Research, University of Iowa, 1976), by Ching Jen Chen and N.C. United States. Army Research Office--Durham (page images at HathiTrust; US access only)
• Unclassified quarterly report of the Reactor Engineering Division. : January 1, 1955 through March 31, 1955. (Argonne National Laboratory, Reactor Engineering Division, 1955), by Argonne National Laboratory (page images at HathiTrust)
• Preliminary physics and heat transfer design calculations for a rocket fuel test reactor (RFTR) (Argonne National Laboratory, Reactor Physics Division, 1964), by D. R. MacFarlane, J. T. Madell, and Argonne National Laboratory (page images at HathiTrust)
• Heat transfer, flow instability and critical heat flux for water in a small tube at 200 psia (Argonne National Laboratory, Reactor Engineering Division, 1963), by R. J. Weatherhead and Argonne National Laboratory (page images at HathiTrust)
• A practical approach to availability and irreversibility (Argonne National Laboratory, Reactor Engineering Division, 1963), by Barton M. Hoglund and Argonne National Laboratory (page images at HathiTrust)
• Proceedings of the AMU-ANL Summer Study Program. : June 19 - Jul 14, 1961. (Argonne National Laboratory, Industrial Hygiene and Safety Division, 1962), by Argonne National Laboratory (page images at HathiTrust)
• Boiling water reactor technology status of the art report : Volume 1. Heat transfer and hydraulics (Argonne National Laboratory, Reactor Engineering Division, 1962), by P. A. Lottes and Argonne National Laboratory (page images at HathiTrust)
• Chemistry Division. (Argonne National Laboratory, Reactor Engineering Division, 1968), by R. D. Carlson, Robert E. Holtz, U.S. Atomic Energy Commission, and Argonne National Laboratory (page images at HathiTrust)
• Two-phase heat transfer with gas injection through a porous boundary surface (Argonne National Laboratory, Reactor Engineering Division, 1964), by A. A. Kudirka and Argonne National Laboratory (page images at HathiTrust)
• Hazard summary report on the Experimental Boiling Water Reactor (EBWR) (Argonne National Laboratory, 1958), by J. M. West and Argonne National Laboratory (page images at HathiTrust)
• Prediction of the critical heat flux in forced convection flow (U.S. Atomic Energy Commission, Division of Technical Information, 1962), by S. Levy, General Electric Company. Atomic Power Equipment Department, and U.S. Atomic Energy Commission (page images at HathiTrust)
• The Graetz problem in cocurrent-flow, double-pipe, heat exchangers (Argonne National Laboratory, Reactor Engineering Division, 1964), by Ralph P. Stein and Argonne National Laboratory (page images at HathiTrust)
• A method of calculating transient temperatures in a multiregion, axisymmetric, cylindrical configuration, the ARGUS program, 1089/RE248, written in FORTRAN II (Argonne National Laboratory, Reactor Physics Division, 1963), by D. F. Schoeberle, L. B. Miller, J. Heestand, and Argonne National Laboratory (page images at HathiTrust)
• Status report on the Argonne Advanced Research Reactor (Argonne National Laboratory, 1961), by D. H. Lennox and Argonne National Laboratory (page images at HathiTrust)
• Temperature rise in a pitted surface (U.S. Atomic Energy Commission. Technical Information Service, 1951), by William Karush, Clinton Laboratories, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heat transfer coefficients with annular flow during "one-through" boiling water to 100 per cent quality at 800, 1100, 1400 PSI ([General Electric Co., Atomic Power Equipment Dept.], 1961), by E. E. Polomik, S. G. Sawochka, S. Levy, U.S. Atomic Energy Commission, and General Electric Company (page images at HathiTrust)
• Axial heat distribution in Brookhaven reactor (United States Atomic Energy Commission, Technical Information Service, 1955), by Melville Clark, Brookhaven National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heat flow from a fin to a boiling liquid (U.S. Atomic Energy Commission. Technical Information Service, 1951), by A. V. Martin, Clinton Laboratories, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heat transfer calculations for the PRTR pressurized gas-cooled loop facility (Hanford Atomic Products Operation, 1961), by J. Muraoka, U.S. Atomic Energy Commission, and Hanford Atomic Products Operation (page images at HathiTrust)
• Temperature rise under uncooled areas of thin plates (U.S. Atomic Energy Commission. Technical Information Division, 1951), by William Karush, Clinton Laboratories, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Determination of burnout limits of polyphenyl coolants : summary report (Aerojet-General Corp. ;, 1958), by T. C. Core, K. Sato, U.S. Atomic Energy Commission. Idaho Operations Office, and Aerojet-General Corporation (page images at HathiTrust)
• Reactor Projects Division (Oak Ridge National Laboratory, 1958), by Lester G. Epel, Oak Ridge National Laboratory, U.S. Atomic Energy Commission, and Union Carbide Corporation (page images at HathiTrust)
• Flow of heat into coating through a narrow strip (U.S. Atomic Energy Commission. Technical Information Division, 1951), by William Karush, G. Young, Clinton Laboratories, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Transient behavior of a natural-circulation loop operating near the thermodynamic critical point (Argonne National Laboratory, Reactor Engineering Division, 1963), by Darrel G. Harden and Argonne National Laboratory (page images at HathiTrust)
• Surface-renewal models for heat transfer between walls and fluidized beds (Argonne National Laboratory, 1967), by R. D. Patel (page images at HathiTrust)
• Condensation of metal vapors: mercury and the kinetic theory of condensation (Argonne National Laboratory, Reactor Engineering Division, 1964), by Donald J. Wilhelm, U.S. Atomic Energy Commission, and Argonne National Laboratory (page images at HathiTrust)
• Application of electron-bombardment heating for boiling liquid metals (Argonne National Laboratory, Reactor Engineering Division, 1964), by R. E. Holtz and Argonne National Laboratory (page images at HathiTrust)
• An evaluation of reactor concepts for use as separate steam superheaters (Argonne National Laboratory, Reactor Engineering Division, 1961), by D. H. Lennox and Argonne National Laboratory (page images at HathiTrust)
• Parallel flow heat transfer to water in open lattic of cylindrical rods (Garden City, Long Island New York : Walter Kidde Nuclear Laboratories, Incorporated 1954., 1954), by Philip Miller and U.S. Atomic Energy Commission. New York Operations Office (page images at HathiTrust)
• Study of effects of turbulence promoters on heat transfer (Oak Ridge, Tennessee : Fairchild Engine and Airplane Corporation, NEPA Division 1950., 1950), by Armour Research Foundation (U.S.), Andrew H. Dowdy, Fairchild Engine and Airplane Corporation, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Boiling pressure drop in rectangular channels (Pittsburgh, Pennsylvania. : Atomic Power Division, Westinghouse Electric Corporation, 1956., 1956), by H. S. Jacket, N. C. Sher, J. D. Roarty, U.S. Atomic Energy Commission, and Westinghouse Electric Corporation. Atomic Power Division (page images at HathiTrust)
• ECCS heat transfer experiences with upper head injection : Volume III, Supplementary information (Pittsburgh, Pennsylvania : Westinghouse Electric Corporation, Nuclear Energy Systems, 1976., 1976), by B. A. McIntyre, U.S. Atomic Energy Commission, and Westinghouse Nuclear Energy Systems (page images at HathiTrust)
• Blowdown experiments with upper head injection in G2 17 x 17 rod array (Pittsburgh, Pennsylvania : Westinghouse Electric Corporation, Nuclear Energy Systems, 1976., 1976), by B. A. McIntyre, U.S. Atomic Energy Commission, and Westinghouse Nuclear Energy Systems (page images at HathiTrust)
• Ex-reactor determination of thermal gap and contact conductance between uranium dioxide, zircaloy-4 interfaces : stage I low gas pressure ([Washington, D.C.] : U.S. Nuclear Regulatory Commission ; [1979]., 1979), by John E. Garnier, Stefan Begej, Pacific Northwest Laboratory. Materials Department. Ceramics and Graphite Section, United States. Department of Energy, and U.S. Nuclear Regulatory Commission (page images at HathiTrust)
• B.W.R. blowdown/emergency core cooling twenty-first quarterly report, January 1 - April 17, 1981 (Washington, D.C. : Division of Accident Evaluation, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1981., 1981), by S. A. Domning, General Electric Company. Nuclear Engineering Division, Electric Power Research Institute, U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Accident Evaluation, United States Government Printing Office, and United States. National Technical Information Service (page images at HathiTrust)
• Startup data report for NRC/PNL Halden Assembly IFA-513. (Washington, D. C. : U.S. Nuclear Regulatory Commission, 1979., 1979), by Donald D. Lanning, Mitchel E. Cunningham, Pacific Northwest Laboratory, and U.S. Nuclear Regulatory Commission (page images at HathiTrust)
• Surface heat transfer from a hot spring fed lake (Dept. of Civil Engineering, Stanford University, 1972), by A. Woodruff Miller, Robert L. Street, and Stanford University. Department of Civil Engineering (page images at HathiTrust; US access only)
• Heat transfer and pressure drop in heat exchangers (The University of Texas, 1943), by Byron Elliott Short (page images at HathiTrust; US access only)
• The electrostatic effect and the heat transmission of a tube (The University, 1941), by Melvin Roland Wahlert and Huber O. Croft (page images at HathiTrust; US access only)
• Some measurements of boiling burn-out (National Advisory Committee for Aeronautics, 1955), by Warren H. Lowdermilk, Walter F. Weiland, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Heat transfer analysis of the LWR pressure vessel steel irradiation capsules in the Oak Ridge Research Reactor-pressure vessel Benchmark Facility (Washington, D. C. : U.S. Nuclear Regulatory Commission : Available from GPO Sales Program, Division of Technical Information and Document Control, U.S. Nuclear Regulatory Commission, 1982., 1982), by Ilana I. Siman-Tov, Oak Ridge National Laboratory. Engineering Technology Division, and U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research (page images at HathiTrust)
• Hydrodynamic instability and thermal convection in a horizontal layer of two immiscible fluids with internal heat generation : final report, July 1975 - June 1980 (Washington, D.C. : U.S. Nuclear Regulatory Commission, 1982., 1982), by F. A. Kulacki, A. T. Nguyen, Ohio State University. Research Foundation, and U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Accident Evaluation (page images at HathiTrust)
• Measurements of a supersonic favorable-pressure-gradient turbulent boundary layer with heat Transfer : part 1 -data compilation. (Silver Spring, Maryland : Naval Ordnance Laboratory, 1973., 1973), by Robert L. P. Voisinet, Roland E. Lee, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Use of phase-change paints to study fin-body interference heating (Silver Spring, Maryland : Naval Surface Weapons Center, White Oak Laboratory, 1976., 1976), by Jr. Gillerlain and Naval Surface Weapons Center. : White Oak Laboratory (page images at HathiTrust)
• Normal impingement of a supersonic jet on a plane : a basic study of shock-interference heating (Silver Spring, Maryland : Naval Surface Weapons Center, White Oak Laboratory, 1975., 1975), by Kuei-Yuan Chien and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• Approximate analysis of heat transfer in transpired boundary layers at limiting Prandtl numbers (Silver Spring, Maryland : Naval Ordnance Laboratory, White Oak, 1974., 1974), by Tse-Fou Zien and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Influence of roughness on heat transfer and transition : ART Program Data Report. (Silver Spring, Maryland. : Naval Ordinance Laboratory, White Oak, 1973., 1973), by R. E. Phinney, F. P. Baltakis, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Boundary-layer transition experiments on pre-ablated graphite nosetips in a hyperballistics range (Silver Spring, Maryland : Naval Surface Weapons Center, White Oak Laboratory, 1976., 1976), by Daniel C. Reda, Robert A. Leverance, and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• MELT-I : a simplified meltdown code for fast reactor safety analysis (Richland, Washington : Battelle Memorial Institute, Pacific Northwest Laboratory, 1968., 1968), by Alan E. Waltar, U.S. Atomic Energy Commission, and Pacific Northwest Laboratory (page images at HathiTrust)
• Reactor systems response analytical development program (Washington, D. C. : Atomic Energy Division, Idaho Operations Office, U.S. Atomic Energy Commission, 1969., 1969), by S. G. Forbes, G. F. Brockett, T. R. Wilson, U.S. Atomic Energy Commission, and Phillips Petroleum Company (page images at HathiTrust)
• Fission product behavior analytical development program (Washington, D. C. : Atomic Energy Division, Idaho Operations Office, U.S. Atomic Energy Commission, 1969., 1969), by S. G. Forbes, G. F. Brockett, R. F. Berger, T. R. Wilson, U.S. Atomic Energy Commission, and Phillips Petroleum Company (page images at HathiTrust)
• Semiscale blowdown and ECC (Washington, D. C. : Atomic Energy Division, Idaho Operations Office, U.S. Atomic Energy Commission, 1969., 1969), by S. G. Forbes, G. F. Brockett, T. R. Wilson, U.S. Atomic Energy Commission, and Phillips Petroleum Company (page images at HathiTrust)
• Scoping emergency cooling heat transfer (SECHT) test project (Washington, D. C. : Atomic Energy Division, Idaho Operations Office, U.S. Atomic Energy Commission, 1969., 1969), by S. G. Forbes, N. K. Sowards, T. R. Wilson, U.S. Atomic Energy Commission, and Phillips Petroleum Company (page images at HathiTrust)
• Pressurized water reactor - full-length emergency cooling heat transfer (PWR-FLECHT) test project (Washington, D. C. : Atomic Energy Division, Idaho Operations Office, U.S. Atomic Energy Commission, 1969., 1969), by S. G. Forbes, N. K. Sowards, T. R. Wilson, U.S. Atomic Energy Commission, and Phillips Petroleum Company (page images at HathiTrust)
• Fuel heatup simulation tests - FHUST (Washington, D. C. : Atomic Energy Division, Idaho Operations Office, U.S. Atomic Energy Commission, 1969., 1969), by S. G. Forbes, G. F. Brockett, T. R. Wilson, U.S. Atomic Energy Commission, and Phillips Petroleum Company (page images at HathiTrust)
• Loft instrument development support program (Washington, D. C. : Atomic Energy Division, Idaho Operations Office, U.S. Atomic Energy Commission, 1969., 1969), by S. G. Forbes, G. F. Brockett, R. F. Berger, R. G. Morrison, T. R. Wilson, U.S. Atomic Energy Commission, and Phillips Petroleum Company (page images at HathiTrust)
• Carolinas Virginia tube reactor (CVTR) in-plant testing project (Washington, D. C. : Atomic Energy Division, Idaho Operations Office, U.S. Atomic Energy Commission, 1969., 1969), by S. G. Forbes, N. K. Sowards, T. R. Wilson, U.S. Atomic Energy Commission, and Phillips Petroleum Company (page images at HathiTrust)
• Fission product sampling and decontamination development program (Washington, D. C. : Atomic Energy Division, Idaho Operations Office, U.S. Atomic Energy Commission, 1969., 1969), by S. G. Forbes, D. R. deBoisblanc, R. F. Berger, T. R. Wilson, U.S. Atomic Energy Commission, and Phillips Petroleum Company (page images at HathiTrust)
• ORNL-LOFT fission product support program (Washington, D. C. : Atomic Energy Division, Idaho Operations Office, U.S. Atomic Energy Commission, 1969., 1969), by S. G. Forbes, W. B. Cottrell, R. F. Berger, T. R. Wilson, U.S. Atomic Energy Commission, and Phillips Petroleum Company (page images at HathiTrust)
• LOFT integral test program (Washington, D. C. : Atomic Energy Division, Idaho Operations Office, U.S. Atomic Energy Commission, 1969., 1969), by S. G. Forbes, R. F. Berger, T. R. Wilson, U.S. Atomic Energy Commission, and Phillips Petroleum Company (page images at HathiTrust)
• The Time-dependent solution to interstitial diffusion in a temperature gradient (Los Alamos, New Mexico : Los Alamos Scientific Laboratory of the University of California, 1972., 1972), by Clarence E. Lee, Terry C. Wallace, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• SECHT III : an experimental investigation of top and bottom flooding of a nuclear bundle simulator (Idaho Falls, Idaho : Idaho Nuclear Corproations, 1970., 1970), by C. M. Moser, R. W. Griebe, U.S. Atomic Energy Commission. Idaho Operations Office, Allied Chemical Corporation, and Aerojet-General Corporation (page images at HathiTrust)
• Survey of the literature pertaining to the phenomena of nucleate boiling (Oak Ridge, Tennessee : USAEC Office of Technical Information Extension, 1959., 1959), by R. A. Rockow, U.S. Atomic Energy Commission. Technical Information Center, and North American Aviation. Atomics International Division (page images at HathiTrust)
• SRE standard operating procedures (Canoga Park, California : Atomics International, A Division of North American Aviation, Inc., 1960., 1960), by R. E. Durand, L. E. Vorderbrueggen, E. N. Pearson, L. L. Johnson, O. G. Jenkins, U.S. Atomic Energy Commission. Technical Information Center, and North American Aviation. Atomics International Division (page images at HathiTrust)
• The S.F.O. code (Schenectady, New York : General Electric Company, Knolls Atomic Power Laboratory, SAR Thermal & Hydraulic Design, 1960., 1960), by J. E. Kalinowski, Knolls Atomic Power Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heat transfer with surface boiling (Oak Ridge, Tennessee : U.S. Atomic Energy Commission, Technical Informaton Service, 1949., 1949), by J. W. Knowles, U.S. Atomic Energy Commission, National Research Council of Canada, and Universit©Øe de Montr©Øeal (page images at HathiTrust)
• Improved heat transfer by application of centrifugal forces (White Plains, New York : Nuclear Development Corportion of America, 1958., 1958), by Kurt Goldman, U.S. Atomic Energy Commission, and Nuclear Development Corporation of America (page images at HathiTrust)
• Heat transfer application of liquid lithium, liquid metals and liquid metal pumps (Livermore, California : University of California, Radiation Laboratory, 1956., 1956), by Frederick E. Frost, Glen Maynard, U.S. Atomic Energy Commission, and Lawrence Radiation Laboratory (page images at HathiTrust)
• Heat transfer in gas-cooled piles (Oak Ridge, Tennessee : U.S. Atomic Energy Commission, Technical Information Service, 1947., 1947), by A. Amorosi, C. Rogers McCullough, U.S. Atomic Energy Commission. Technical Information Service, and Oak Ridge National Laboratory (page images at HathiTrust)
• Heat transfer to a boiling liquid : mechanism and correlations, progress report no. 7 (Los Angeles, California : Department of Engineering, University of California, 1958., 1958), by Kurt Walter Forster, R. Greif, Los Angeles. Department of Engineering University of California, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Heat transfer and frictional effects in laminar boundary layers : Part 5. The modified Lighthill Method for determining the rate of heat transfer (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1954, 1954), by Arthur N. Tifford, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Ohio State University. Research Foundation (page images at HathiTrust)
• An experimental study of the interaction of strong sound fields with free convection boundary layers (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), by Arthur L. Sprott, Frederick L. Durand, Jack P. Holman, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
• Survey of boundary layer heat transfer at high velocities and high temperatures (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1960., 1960), by E. R. G. Eckert, United States. Air Force. Air Research and Development Command, Wright Air Development Center, University of Minnesota, and United States. Department of the Air Force. Wright Air Development Center (page images at HathiTrust)
• Survey on heat transfer at high speeds (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1954, 1954), by E. R. G. Eckert, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
• An Experimental study of the effects of non-uniform wall temperature on heat transfer in laminar and turbulent axisymmetric flow along a cylinder (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by R. Eichhorn, A. D. Anderson, E. R. G. Eckert, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
• Exact solution of laminar heat transfer in wedge-shaped passages with various boundary conditions (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1957., 1957), by J. T. Yen, United States. Air Force. Air Research and Development Command, University of Minnesota, Heat Transfer Laboratory, and Wright Air Development Center (page images at HathiTrust)
• Heat transfer to boundary layers with pressure gradients (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by Ralph Alois Seban, Hugh Won Chan, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Berkeley University of California (page images at HathiTrust)
• Simplified procedures for the calculation of heat transfer to surfaces with non-uniform temperatures (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1956., 1956), by J. P. Hartnett, R. L. Sampson, Roland Birkebak, E. R. G. Eckert, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and University of Minnesota. Department of Mechanical Engineering. Heat Transfer Laboratory (page images at HathiTrust)
• An investigation of laminar, transitional and turbulent heat transfer on blunt-nosed bodies in hypersonic flow (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), by Robert J. Cresci, Paul A. Libby, Donald A. MacKenzie, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Polytechnic Institute of Brooklyn. |b Department of Aerospace Engineering and Applied Mechanics (page images at HathiTrust)
• Turbulent heat transfer on blunt-nosed bodies in two-dimensional and general three-dimensional hypersonic flow (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by Roberto Vaglio-Laurin, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Polytechnic Institute of Brooklyn. Department of Aeronautical Engineering and Applied Mechanics (page images at HathiTrust)
• The effect of centrifugal forces on boundary layer transition for a highly heated body (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), by Eugene Sevigny, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Polytechnic Institute of Brooklyn. Department of Aerospace Engineering and Applied Mechanics (page images at HathiTrust)
• Thermal protection of structural, propulsion, and temperature-sensitive materials for hypersonic and space flight (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1960., 1960), by William P. Manos, Anthony J. Tuzzolino, Donald E. Taylor, Wright Air Development Center, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Transient analysis of heat conduction through a slab by infinite series (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966), by Thomas N. Bernstein, Robert M. Engle, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Electrofluidmechanics : a study of electrokinetic actions in fluids (Wright-Patterson Air Force Base, Ohio : Propulsion Laboratory, Aeronautical Systems Division, Air Force Systems Command, [1962], 1962), by Henry R. Velkoff and United States. Air Force. Systems Command. Aeronautical Systems Division. Propulsion Laboratory (page images at HathiTrust)
• An experimental study of the distribution of convective heat transfer to a large-scale model of parachute cloth (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), by E. R. G. Eckert, K. M. Krall, C. J. Scott, M. Ruiz-Urbieta, J. E. Anderson, Wright-Patterson Air Force Base (Ohio), University of Minnesota, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Heat transfer to surfaces in the neighborhood of protuberances in hypersonic flow (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1957., 1957), by M. H. Bloom, Adrian Pallone, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Polytechnic Institute of Brooklyn (page images at HathiTrust)
• Pressure and heat transfer measurements for hypersonic flows over expansion corners and ahead of ramps (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1963), by Louis G. Kaufman, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command. Aeronautical Systems Division, and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Pressure and laminar heat transfer results in three-dimensional hypersonic flow (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by Victor Zakkay, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Polytechnic Institute of Brooklyn. Department of Aeronautical Engineering and Applied Mechanics (page images at HathiTrust)
• Thermal analysis of a superconducting generator (Wright-Patterson Air Force Base, Ohio : Transmission Technology Section, Flight Vehicle Power Section, Flight Accessories Laboratory, Aeronautical Systems Division, United States Air Force, 1962., 1962), by Robert J. Smith and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Inhibition of flow separation at high speed. Volume 2, Calculation of nonadiabatic laminar boundary layers (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), by Frederick K. Goodwin, Larry L. Lynes, Jack Norman Nielsen, Air Force Flight Dynamics Laboratory (U.S.), and Nielsen Engineering & Research (page images at HathiTrust)
• Inhibition of flow separation at high speed. Volume 3, Experimental results for laminar boundary layers (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), by Jack Norman Nielsen, Frederick K. Goodwin, Larry L. Lynes, Air Force Flight Dynamics Laboratory (U.S.), and Nielsen Engineering & Research (page images at HathiTrust)
• Shroud tests of pressure and heat transfer over short afterbodies with separated wakes (Wright-Patterson Air Force Base, Ohio. Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by Martin H. Bloom, Adrian Pallone, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Polytechnic Institute of Brooklyn. Department of Aeronautical Engineering and Applied Mechanics (page images at HathiTrust)
• Evaluation of several hypersonic turbulent heat transfer analyses by comparison with experimental data (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research Development and Command, United States Air Force, 1957., 1957), by Paul A. Libby, Robert J. Cresci, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Polytechnic Institute of Brooklyn. |b Department of Aerospace Engineering and Applied Mechanics (page images at HathiTrust)
• The use of helium for cooling nozzles exposed to high temperature gas streams (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1955., 1955), by Antonio Ferrie, Paul A. Libby, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Polytechnic Institute of Brooklyn (page images at HathiTrust)
• Investigation of the thermal properties of high-temperature insulation materials (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by A. E. Wechsler, Peter E. Glaser, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command. Aeronautical Systems Division, Inc Arthur D. Little, Wright-Patterson Air Force Base (Ohio), and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
• Space radiator analysis and design : Part 1 (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), by Donald Bawden Mackay, C. P. Bacha, United States. Air Force. Systems Command. Aeronautical Systems Division, Inc. Space and Information Systems Division North American Aviation, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Transient heat transfer in laminar flow in the entrance region of tubes with heat capacity (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), by Vedat S. Arpaci, Wright Air Development Center, United States. Air Force. Air Research and Development Command, and Massachusetts Institute of Technology. Heat Transfer Laboratory (page images at HathiTrust)
• Heat-transfer studies (Wright Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1959., 1959), by T. C. Core, K. Sato, B. Misra, J. F. Harkee, Aerojet-General Corporation, United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Model instrumentation techniques for heat transfer and force measurements in a hypersonic shock tunnel (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research Development and Command, United States Air Force, 1956., 1956), by R. J. Vidal, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Investigation of the para-ortho shift of hydrogen (Wright-Patterson Air Force Base, Ohio : Air Force Aero-Propulsion Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1963., 1963), by R. G. Clark, G. E. Schmauch, A. Jambhekar, J. F. Kucirka, United States. Air Force. Systems Command. Aeronautical Systems Division, and inc Air Products and Chemicals (page images at HathiTrust)
• Space radiator analysis and design : Part 2 (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1962), by Donald Bawden Mackay, United States. Air Force. Systems Command. Aeronautical Systems Division, Inc. Space and Information Systems Division North American Aviation, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Transient heat flow across unidirectional fibers in composites (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), by Lit S. Han, Moshen Bashizadeh-Fakhar, Air Force Flight Dynamics Laboratory (U.S.), and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Further data on the juncture condition of temperature at the interface of two bodies in sliding contact (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1963., 1963), by T. E. Simkins, S. L. Pu, Rensselaer Polytechnic Institute, United States. Air Force. Systems Command. Aeronautical Systems Division, and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
• Condensation heat transfer. Part II, Solution of the film condensation problem by successive analytical iteration (Wright-Patterson Air Force Base, Ohio : Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, 1963., 1963), by Jon H. Lee and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Regulation of cutaneous circulation during body heating (Wright-Patterson Air Force Base, Ohio : Biomedical Laboratory, Aerospace Medical Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by Alrick B. Hertzman, Aerospace Medical Laboratory (U.S.), St. Louis University, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Inhibition of flow separation at high speed. Volume IV, Calculation of nonadiabatic laminar boundary layers on conical compression surfaces (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), by Frederick K. Goodwin, Larry L. Lynes, Air Force Flight Dynamics Laboratory (U.S.), and Nielsen Engineering & Research (page images at HathiTrust)
• Experimental verification of the analyses and computer programs concerning heat transfer through semitransparent materials (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), by H. Finch, C. Moeller, M. Noland, Air Force Flight Dynamics Laboratory (U.S.), and Mo.) Midwest Research Institute (Kansas City (page images at HathiTrust)
• Thermal properties of materials at elevated temperatures (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), by Herbert W. Deem, Charles F. Lucks, Webster D. Wood, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Battelle Memorial Institute (page images at HathiTrust)
• Investigation of materials for mechanical transmission of deflections at elevated temperatures (Wright-Patterson Air Force Base, Ohio : Directorate of Engineering Test, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by J. S. Islinger, Edward L. McDowell, United States. Air Force. Systems Command. Aeronautical Systems Division, and Armour Research Foundation (U.S.) (page images at HathiTrust)
• Literature survey on liquid metal boiling (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1961), by Richard E. Balzhiser, Andrew S. Teller, Herman Merte, C. Phillip Colver, Lowell R. Smith, Edward E. Hucke, John A. Clark, United States. Air Force. Systems Command. Aeronautical Systems Division, and University of Michigan. Department of Chemical and Metallurgical Engineering (page images at HathiTrust)
• Procedure used for X-15 heat transfer and pressure distribution tests at hypersonic speeds (Wright-Patterson Air Force Base, Ohio : Arnold Engineering Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), by J. A. Durand, J. P. Rhudy, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Catalytic surface recombination in boundary-layer profiles of the Falkner-Skan type (Washington, D.C. : Air Force Office of Scientific Research, United States Air Force, 1962., 1962), by William J. Rae, United States. Air Force. Office of Scientific Research, and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Aerodynamic heating and heat transfer phenomena at Mach numbers 3 to 4 (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Equipment Laboratory, Air Research and Development Command, United States Air Force, 1951., 1951), by K. G. Anderson, J. M. Durben, H. B. Merrell, Wright Air Development Center, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Low-density stagnation-point heat transfer in hypersonic air flow (Wright-Patterson Air Force Base, Ohio : Aeronautical Research Laboratory, Air Force Research Division, Air Research and Development Command, United States Air Force, 1961., 1961), by Charles F. Wittliff, Merle R. Wilson, Aerospace Research Laboratories (U.S.), and Cornell Aeronautical Laboratory (page images at HathiTrust)
• A Study of aerodynamic effects of isothermal and temperature gradient atmospheres on reentry trajectories (Washington, D.C. : Air Force Office of Scientific Research, United States Air Force, 1962., 1962), by Leo Rute, United States. Air Force. Office of Scientific Research, and Polytechnic Institute of Brooklyn. Department of Aeronautical Engineering and Applied Mechanics (page images at HathiTrust)
• Pressure and heat transfer measurements for Mach 8 flows over a blunt pryamidal configuration with aerodynamic controls. Part I. Pressure data for delta wing surface (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), by Louis G. Kaufman, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Research on the effects of collisions of small particles with bodies moving at hypersonic speed. PART II Erosion and heat transfer effects (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), by G. Whitnah, D. Rosenberg, W. Torgeson, Arie Gaalswyk, J. Upton, G. Wehner, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Inc General Mills (page images at HathiTrust)
• A Study of laminar heat transfer to spherically blunted cones and hemisphere-cylinders at hypersonic conditions (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), by B. J. Griffith, Clark H. Lewis, Inc. AEDC Division Sverdrup/ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• Handbook of supersonic aerodynamics. Volume 5, Sections 13 & 14. Viscosity and heat transfer effects (White Oak, Maryland : U.S. Naval Ordnance Laboratory, Aeroballistics, 1966., 1966), by R. E. Wilson, Md.) Naval Ordnance Laboratory (White Oak, and Johns Hopkins University. Applied Physics Laboratory (page images at HathiTrust)
• Pressure measurements for mach five flows over winged re-entry configurations with aerodynamic controls. Part II. Conical cabin configuration (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), by Louis G. Kaufman, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation (page images at HathiTrust)
• Pressure and laminar heat transfer distribution at the nose region of a semicircular toroid at M₀₀ = 3 and 8 (Wright-Patterson Air Force Base, Ohio : Aeronautical Research Laboratories, Air Force Research Division, Air Research and Development Command, United States Air Force, 1960., 1960), by Victor Zakkay, Marian Visich, United States. Air Force. Aeronautical Research Laboratories, and Polytechnic Institute of Brooklyn. Department of Aeronautical Engineering and Applied Mechanics (page images at HathiTrust)
• A theoretical analysis of heat transfer in regions of reverse flow (Princeton, New Jersey : Princeton University, Department of Aeronautical Engineering, 1963., 1963), by R. W. Garvine, United States. Air Force. Office of Scientific Research, and Princeton University. Department of Aeronautical Engineering (page images at HathiTrust)
• Temperatures in structures. Part I, General discussion and one-dimension, one-layer problem; analytic solutions (China Lake, California : U. S. Naval Ordnance Test Station, Research Department, 1957., 1957), by Charles J. Thorne, United States. Navy Department. Bureau of Ordnance, and Calif.) Naval Ordnance Test Station (China Lake (page images at HathiTrust)
• Heat transfer correlations for blunt cones at angle of attack (Los Angeles, California : Space and Missile Systems Organization, Air Force Systems Command, United States Air Force, 1971., 1971), by George F. Widhopf, United States. Air Force. Systems Command, Space and Missile Systems Organization (U.S.), and Aerospace Corporation (page images at HathiTrust)
• Standardization of symbols and units for environmental research (Wright-Patterson Air Force Base, Ohio : Aerospace Medical Research Laboratories, Aerospace Medical Division, Air Force Systems Command, United States Air Force, 1966., 1966), by W. C. Kaufman and Aerospace Medical Research Laboratories (U.S.) (page images at HathiTrust)
• Studies on heat transfer in laminar free convection with the Zehnder-Mach Interferometer (Wright-Patterson Air Force Base, Ohio : United States, Air Force, Air Materiel Command, 1948, 1948), by E. R. G. Eckert, E. E. Soehngen, and United States. Air Force. Air Matériel Command (page images at HathiTrust)
• A series solution to the laminar heat transfer problem at hypersonic speeds (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by Hung-Ta Ho, Ronald F. Probstein, United States. Air Force. Air Research and Development Command, Aerospace Research Laboratories (U.S.), and Brown University. Division of Engineering (page images at HathiTrust)
• Stability theory for cross hatching. Part I, Linear stability theory (Norton Air Force Base, California : Space and Missile Systems Organization, Air Force Systems Command, United States Air Force, 1972., 1972), by Lester Lees, Denny R. S. Ko, T. Kubota, United States. Air Force. Systems Command, Space and Missile Systems Organization (U.S.), and California Institute of Technology (page images at HathiTrust)
• Applied heat transfer course lecture notes on interference flows (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Flight Mechanics Division, High Speed Aero Performance Branch, Air Force Systems Command, United States Air Force, 1972., 1972), by Gerald L. Burke and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Some heat transfer problems in hypersonic flow ([Brooklyn, New York] : Polytechnic Institute of Brooklyn, Department of Aeronautical Engineering and Applied Mechanics, [1959], 1959), by Antonio Ferri, United States. Air Force. Air Research and Development Command, and Polytechnic Institute of Brooklyn (page images at HathiTrust)
• Experimental laminar heat transfer from an oscillating flat plate (Washington, D. C. : United States Air Force, Air Force Office of Scientific Research, 1963., 1963), by N. A. Evans, Princeton University. Department of Aeronautical Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Pressure measurements for mach five flows over winged re-entry configurations with aerodynamic controls. Part 1. Blunt cabin configuration (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), by Louis G. Kaufman, Air Force Flight Dynamics Laboratory (U.S.), Wright-Patterson Air Force Base. Flight Dynamics Laboratory. Research and Technology Division, and Grumman Aircraft Engineering Corporation (page images at HathiTrust)
• The theory of radiation cooling at high Mach numbers (Princeton, New Jersey : AeroChem Research Laboratories, Inc., 1960., 1960), by Daniel E. Rosner, AeroChem Research Laboratories, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Nonequilibrium hypersonic stagnation flow at low reynolds numbers (Los Angeles, California : Ballistic Systems and Space Systems Divisions, Los Angeles Air Force Station, Air Force Systems Command, United States Air Force, 1964., 1964), by G. I. Inger, United States. Air Force. Systems Command. Space Systems Division, and Aerospace Corporation. Laboratory Operations (page images at HathiTrust)
• Boundary layer transition at supersonic speeds : three dimensional roughness effects (spheres) (Washington, D.C. : Air Force Office of Scientific Research, United States Air Force, 1961., 1961), by E. R. Van Driest, C. B. Blumer, United States. Air Force. Office of Scientific Research, and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
• Interaction of chemistry, turbulence and shock waves in hypervelocity flow (Pasadena, California : California Institute of Technology, 1994., 1994), by G. V. Candler, B. Sturtevant, D. Pullin, B. V. McKoy, D. Meiron, A. Leonard, H. Hornung, P. Dimotakis, California Institute of Technology, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Homogeneous boundary layer at an axisymmetric stagnation point with large rates of injection (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1960., 1960), by Paul A. Libby, United States. Air Force. Air Research and Development Command, Polytechnic Institute of Brooklyn. Aerodynamics Laboratory, and United States. Wright Air Development Division (page images at HathiTrust)
• Thermophysical properties of thermal energy storage materials - Aluminum (L.G. Hanscom Field, Massachusetts : Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1973., 1973), by Clare C. Leiby, Thomas G. Ryan, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Studies on the structure of turbulence (Cambridge, Massachusetts : Geophysics Research Directorate, Air Force Cambridge Research Center, Air Research and Development Command, United States Air Force, 1958., 1958), by J. A. Businger, Hans A. Panofsky, Verner Suomi, University of Wisconsin. Department of Meteorology, and Air Force Cambridge Research Center (U.S.). Geophysics Research Directorate (page images at HathiTrust)
• Theoretical and experimental studies of hypersonic viscous effects (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1965., 1965), by Clark H. Lewis, Jack D. Whitfield, United States. Air Force. Arnold Air Force Base, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• Experimental studies on the interaction of strong sound fields with free convection boundary layers (Wright-Patterson Air Force Base, Ohio : Aeronautical Research Laboratory, Air Force Research Division, Air Research and Development Command, United States Air Force, 1960., 1960), by E. E. Soehngen, J. P. Holman, and Aerospace Research Laboratories (U.S.) (page images at HathiTrust)
• Subsonic flow of hot gas through a highly cooled constant-area channel (Los Angeles, California : Space and Missile Systems Organization, Los Angeles Air Force Station, Air Force Systems Command, United States Air Force, 1967., 1967), by Harold Mirels, United States. Air Force. Systems Command, Space and Missile Systems Organization (U.S.), and Aerospace Corporation (page images at HathiTrust)
• The effects of resonant acoustic vibrations on the local and overall heat transfer coefficients for air flowing though an isothermal horizontal tube (Wright-Patterson Air Force Base, Ohio : Aeronautical Research Laboratory, Air Force Research Division, Air Research and Development Command, United States Air Force, 1960., 1960), by Thomas Woodrow Jackson, Harold L. Johnson, Calvin C. Oliver, Kenneth R. Purdy, Aerospace Research Laboratories (U.S.), and Georgia Institute of Technology (page images at HathiTrust)
• Laminar, transitional, and turbulent heat transfer measurements on a yawed blunt conical nosetip (Los Angeles, California : Space and Missile Systems Organization, Los Angeles Air Force Station, Air Force Systems Command, United States Air Force, 1972., 1972), by George F. Widhopf, United States. Air Force. Systems Command, Space and Missile Systems Organization (U.S.), and Aerospace Corporation (page images at HathiTrust)
• Solution for the transient one-dimensional heat conduction in an infinite slab (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), by John T. Miller, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Studies of transient heat conduction at high thermal flux (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, U.S. Air Force, 1961., 1961), by H. Norman Abramson, John C. Cook, Wen-Hwa Chu, United States. Air Force. Air Research and Development Command, United States. Wright Air Development Division, and Southwest Research Institute (page images at HathiTrust)
• Some mass transfer effects on the wall jet (Washington, D.C. : Air Force Office of Scientific Research, United States Air Force, 1962., 1962), by Herbert Fox, Martin H. Steiger, United States. Air Force. Office of Scientific Research, and Polytechnic Institute of Brooklyn. Department of Aerospace Engineering and Applied Mechanics (page images at HathiTrust)
• Experimental heat transfer to blunt axisymmetric bodies near the limit of continuum flow (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1962., 1962), by J. Leith Potter, John T. Miller, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• The Heat transfer and fluid dynamics of concave surface curvature (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1988., 1988), by P. Bradshaw, R. L. Moffat, J. P. Johnston, Stanford University. Department of Mechanical Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• The effect of transverse vibrations on the heat-transfer rate from a heated vertical plate in free convection (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1957, 1957), by Andrew Joseph Shine, Wright Air Development Center, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Digital computer solution of complex transient heat transfer problems ([Morgantown, W. Va.] : [West Virginia University], [1956?], 1956), by J. T. Anderson, W. K. Koffel, and J. M. Botje (page images at HathiTrust; US access only)
• Heat transfer and pressure drop during viscous flow across unbaffled tube banks (Newark, Del., 1950), by Olaf Preysz Bergelin (page images at HathiTrust; US access only)
• Laminar, transitional, and turbulent heat transfer to a cone-cylinder-flare body at Mach 8.0 (Air Force Office of Scientific Research, United States Air Force, 1962), by Victor Zakkay, Clifton J. Callahan, Polytechnic Institute of Brooklyn. Dept. of Aerospace Engineering and Applied Mechanics, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• A study of aerodynamic effects of isothermal and temperature gradient atmospheres on reentry trajectories (Polytechnic Institute of Brooklyn, 1962), by Leo Rute and Polytechnic Institute of Brooklyn. Dept. of Aerospace Engineering and Applied Mechanics (page images at HathiTrust; US access only)
• On the solution of heat conduction problems in a melting solid. (Defense Technical Information Center, 1960), by Bruno A. Boley and Columbia Univ. New York Inst. of Flight Structures (page images at HathiTrust; US access only)
• On the conduction of heat in a melting slab. (Defense Technical Information Center, 1961), by Stephen J. Citron and Columbia Univ. New York Dept. of Civil Engineering and Engineering Mechanics (page images at HathiTrust; US access only)
• Upper and lower bounds for the solution of a melting problem. (Defense Technical Information Center, 1962), by Bruno A. Boley and Columbia Univ. New York Inst. of Flight Structures (page images at HathiTrust; US access only)
• Transient coupled thermoplastic boundary value problems in the half-space. (Defense Technical Information Center, 1961), by Irwin S. Tolins, Bruno A. Boley, and Columbia Univ. New York Inst. of Flight Structures (page images at HathiTrust; US access only)
• Transient temperature distributions in a sphere due to aerodynamic heating (Polytechnic Institute of Brooklyn, 1959), by Frederick V. Pohle, J. L. Boccio, and Polytechnic Institute of Brooklyn (page images at HathiTrust; US access only)
• A note on the transient temperature distribution in an orthotropic sphere due to aerodynamic heating (Polytechnic Institute of Brooklyn, 1961), by B. Venkatraman, Frederick V. Pohle, Sharad A. Patel, and Polytechnic Institute of Brooklyn (page images at HathiTrust; US access only)
• Comparison of the experimental and theoretical distributions of lift on a slender inclined body of revolution at M = 2 (NACA, 1953), by Edward W. Perkins, Donald M. Kuehn, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
• Measurements of aerodynamic heat transfer and boundary-layer transition on a 10° cone in free flight at supersonic Mach numbers up to 5.9 (NACA, 1956), by Charles B. Rumsey, Dorothy B. Lee, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Experimental study of vane heat transfer and aerodynamics at elevated levels of turbulence (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1994), by Forrest E. Ames and Lewis Research Center (page images at HathiTrust)
• Heat transfer from water flowing through a chilled-bed open channel (United States Government Printing Office, 1990), by Paul W. Richmond, Virgil J. Lunardini, Cold Regions Research and Engineering Laboratory (U.S.), and United States Army Corps of Engineers (page images at HathiTrust)
• Natural convection heat transfer in water near its density maximum (United States Government Printing Office, 1990), by Yin-Chao Yen, United States Army Corps of Engineers, and Cold Regions Research and Engineering Laboratory (U.S.) (page images at HathiTrust)
• Pressure measurements for Mach 8 flows over expansion corners and ramps on an internally cooled model. Part 2. Flows over a flat plate with and without a partial span ramp : part of an investigation of hypersonic flow separation and control characteristics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), by Louis G. Kaufman, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Pressure measurements for Mach 8 flows over expansion corners and ramps on an internally cooled model. Part 3 Flows over full span ramps mounted on a flat plate (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), by Louis G. Kaufman, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Heat transfer measurements at Mach 8 on an aerodynamically controllable winged re-entry configuration : part of an investigation of hypersonic flow separation and control characteristics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), by Lawrence Meckler, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Final report on study of heat transfer through refractory lined gasifier vessel walls (The Division ;, 1979), by United States. Department of Energy. Division of Planning and Systems Engineering, J. Richard Schorr, and Battelle Memorial Institute. Columbus Laboratories (page images at HathiTrust; US access only)
• Surface temperature measurements with thermoelectric materials (Wright-Patterson Air Force Base, Ohio : Directorate of Engineering Test, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by W. Lai, United States. Air Force. Systems Command. Aeronautical Systems Division, and Stanford Research Institute (page images at HathiTrust)
• Heat loss calculations. (U.S. Dept. of Housing and Urban Development, 1968), by United States Federal Housing Administration (page images at HathiTrust)
• Research on nonisentropic gas dynamics (Cornell Aeronautical Laboratory of Cornell University, 1970), by Robert J. Vidal, Gordon E. Merritt, John A. Bartz, United States. Air Force. Office of Scientific Research, and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Heat transfer and flow friction characteristics of several plate-fin type compact heat exchanger surfaces (Naval Postgraduate School, 1967), by Paul F. Pucci, R. E. Traister, S. F. Ball, and Naval Postgraduate School (U.S.) (page images at HathiTrust)

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