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Heat -- Transmission

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• Heat
• Energy transfer
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• Transmission

• Heat -- Transmission -- Experiments
• Heat -- Transmission -- Instruments
• Heat -- Transmission -- Periodicals
• Ablation (Aerothermodynamics)
• Film boiling
• Film coefficients (Physics)
• Heat exchangers
• Heat flux
• Heat pipes
• Heat pulses
• Heat sinks (Electronics)
• Heat-transfer media
• Rayleigh number
• Reynolds analogy
• Terrestrial heat flow
• Thermal boundary layer

• Heat transfer
• Thermal transfer
• Transmission of heat

• 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)
• Calculation of compressible turbulent boundary layers with pressure gradients and heat transfer / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by Larry L. Lynes, Gary D. Kuhn, Jack Norman Nielsen, Nielsen Engineering & Research, and Ames Research Center (page images at HathiTrust)
• Experimental data on stagnation-point gas injection cooling on a hemisphere-cone in a hypersonic arc tunnel / (Washington, D.C. : National Aeronautics and Space Administration ; Washington, D.C. : For sale by the Office of Technical Services, Department of Commerce [distributor], 1964), by John E. Grimaud, Leonard C. McRee, and Langley Research Center (page images at HathiTrust)
• Conditioning and steady-state performance of SNAP-8 tube-in-shell mercury boiler / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 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 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1966), by Michael B. Weinstein and Lewis Research Center (page images at HathiTrust)
• Experimental feasibility study of water-filled capillary-pumped heat-transfer loops / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1966), by Francis J. Stenger and Lewis Research Center (page images at HathiTrust)
• Experimental study of effect of simulated reactor core position on nozzle heat transfer / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1966), by James F. Schmidt and Lewis Research Center (page images at HathiTrust)
• Vacuum chamber heat-transmission analysis / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1967), by Walter W. Guy, Wilbert E. Ellis, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Calculation of turbulent boundary layers with heat transfer and pressure gradient utilizing a compressibility transformation. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 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. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 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/ (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1971), by Ellsworth E. Gerrels, Robert E. Killen, Lewis Research Center, and General Electric Company (page images at HathiTrust)
• 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° / (Washington, [D.C.] : 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)
• Aerodynamic performance of a fully film cooled core turbine vane tested with cold air in a two-dimensional cascade / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1975), by Roy G. Stabe, John F. Kline, and Lewis Research Center (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 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1966), by John J. Bertin and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Water table tests of proposed heat transfer tunnels for small turbine vanes / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by Peter L. Meitner and Lewis Research Center (page images at HathiTrust)
• Dynamic response of high-frequency pressure transducers to large amplitude sinusoidal pressure oscillations / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1972), by Richard E. Robinson, Lewis Research Center, and Battelle Memorial Institute (page images at HathiTrust)
• Free flight observation of a separated turbulent flow including heat transfer up to Mach 8.5 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Dudley George McConnell and Lewis Research Center (page images at HathiTrust)
• Wind tunnel investigation of simulated helicopter engine exhaust interacting with windstream / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by Craig S. Shaw, John C. Wilson, and Langley Research Center (page images at HathiTrust)
• Observation of flow excursions in a simulated gas-cooled reactor passage / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1970), by Paul Vingerhoet, Eli Reshotko, Edward R. Kolbe, Lewis Research Center, and Case Western Reserve University (page images at HathiTrust)
• Analysis of the transient radiation heat transfer of an uncooled rocket engine operating outside Earth's atmosphere / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by William H. Robbins and Lewis 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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1959]), by Francis S. Stepka, Hadley T. Richards, 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 / (Washington, [D.C.] : 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 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Richard A. Hord and Langley Research Center (page images at HathiTrust)
• FREE-FLIGHT AERODYNAMIC-HEATING DATA TO MACH NUMBER 10.4 FOR A MODIFIED VON KARMAN NOSE SHAPE. (Ft. Belvoir Defense Technical Information Center, MAY 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)
• Reactor systems response analytical development program /, 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 /, 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 /, 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 /, 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 /, 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 /, 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 /, 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 /, 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 /, 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 /, 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 /, by S. G. Forbes, R. F. Berger, T. R. Wilson, U.S. Atomic Energy Commission, and Phillips Petroleum Company (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)
• A mathematical model of the evolution of radiation fog /, by I. M Zakharova and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)

• Experimental Results of a Heat-Transfer Study from a Full-Scale Pebble-bed Heater (NASA Technical Note D-265; Washington: National Aeronautics and Space Administration, 1960), by Richard B. Lancashire, Erwin A. Lezberg, and James F. Morris (page images at HathiTrust)

• Latin American Applied Research (partial serial archives)

• Experimental investigation of the feasibility of ablation-cooling a rocket nozzle with possible application to solid-propellant engines / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Richard R. Cullom and Lewis Research Center (page images at HathiTrust)
• Qualitative measurements of the effective heats of ablation of several materials in supersonic air jets at stagnation temperatures up to 11,000À F / (Washington, D.C. : NACA, 1958), by Bernard Rashis, Russell N. Hopko, William G. Witte, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• An analysis of the coupled chemically reacting boundary layer and charring ablator, (Washington, D.C., National Aeronautics and Space Administration, 1968), by Itek Corporation. Vidya Division, Carl B. Moyer, Roald A. Rindall, Eugene P. Bartlett, and Robert M. Kendall (page images at HathiTrust)
• An experimental investigation of ablating materials at low and high enthalpy potentials / (Washington [D.C.] : National Aeronautics and Space Administration, [1960]), by Bernard Rashis, Thomas E. Walton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Stagnation point analysis of coupled viscous-radiating flow with massive blowing / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1970), by K. H. Wilson, Ames Research Center, and Lockheed Aircraft Corporation (page images at HathiTrust)
• Study of critical defects in ablative heat shield systems for the space shuttle / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1972), by R. L. Thompson, W. E. Driver, Ward D. Rummel, Langley Research Center, and Martin Marietta Denver Aerospace (page images at HathiTrust)
• Advanced methods for calculating radiation transport in ablation-product contaminated boundary layers / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1970), by William E. Nicolet, Langley Research Center, and Aerotherm Corporation (page images at HathiTrust)
• An analysis of ablation-shield requirements for manned reentry vehicles / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1960), by Leonard Roberts, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic evidence pertaining to the entry of tektites into the earth's atmosphere / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1962), by Dean R. Chapman, Lewis A. Anderson, Howard K. Larson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight and ground tests of a very-low-density elastomeric ablative material / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by George C. Olsen, Andrew Chapman, and Langley Research Center (page images at HathiTrust)
• Effects of material composition on the ablation performance of low-density elastomeric ablators / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Stephen S. Tompkins, Walter P. Kabana, and Langley Research Center (page images at HathiTrust)
• Two-dimensional analysis of heat and mass transfer in porous media using the strongly implicit procedure / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Donald M. Curry and Lyndon B. Johnson Space Center (page images at HathiTrust)
• Apollo experience report : thermal protection subsystem / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by James E. Pavlosky, Leslie G. St. Leger, and Lyndon B. Johnson Space Center (page images at HathiTrust)
• Deployable centrifugally stabilized structures for atmospheric entry from space / (Washington : National Aeronautics and Space Administration : Springfield, Va. : for sale by the National Technical Information Service, 1964), by H. U. Schuerch, R. MacNeal, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Attached and separated boundary layers on highly cooled, ablating and nonablating models at M=13.8 / ([Washington, D.C.] : National Aeronautics and Space Administration ; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., [1967]), by Donald M. Kuehn and Daryl J. Monson (page images at HathiTrust)
• Comparison of the aerodynamic characteristics of an ablating and nonablating blunted conical body / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Robert L. Kruse and Ames Research Center (page images at HathiTrust)
• An analysis of a charring ablator with thermal nonequilibrium, chemical kinetics, and mass transfer / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Ronald K. Clark and Langley Research Center (page images at HathiTrust)
• Parametric study of a low-density charring ablator / (Washington, D.C. : National Aeronautics and Space Administration [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia], 1966), by Stephen S. Tompkins, Marvin B. Dow, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analytical determination of the effect of thermal property variations on the performance of a charring ablator / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966), by C. M. Pittman, William D. Brewer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Tables of meteor ablation /, by M. Gadsden and Institute for Telecommunication Sciences and Aeronomy (U.S.) (page images at HathiTrust)
• The carbon-carbon assessment program : appendix B, 50 MW ablation testing and results : [final report, May 73-March 74] / (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1975), by Robert E Maurer, C A Powars, and Acurex Corporation. Aerotherm Division (page images at HathiTrust)
• Microstructural assessment of the series M 50MW ramp materials : final report for period April 1975 - June 1977 / (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1978), by Ala.) Southern Research Institute (Birmingham and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
• Comparison of measurements of internal temperatures in ablation material by various thermocouple configurations / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, Washington, D.C. 20230], 1964), by Marvin B. Dow, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Analysis of charring ablation with description of associated computing program, (Washington, National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by Fred W. Matting (page images at HathiTrust; US access only)
• Simulation in ground-test facilities of ablation performance of charring ablators during atmospheric entry / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Stephen S. Tompkins, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• An experimental study of a carbon-phenolic ablation material / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Kenneth Sutton, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Entry thermal protection. (Washington : National Aeronautics and Space Administration, 1968), by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The effect of asymmetric ablation on trim angle of attack / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Robert L. Kruse and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Aerothermal test results from the first flight of the Pegasus air-launched space booster / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by Gregory Noffz and Dryden Flight Research Facility (page images at HathiTrust)
• Pressure and heat-transfer distributions in a simulated wing-elevon cove with variable leakage at a free-stream Mach number of 6.9 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1978), by William D. Deveikis, Whitney Bartlett, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Apparatus for experimental investigation of aerodynamic radiation with absorption by ablation products / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by William L. Wells, W. L. Snow, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance of an ablator for space shuttle in-orbit repair in an arc-plasma airstream / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], [1983]), by David A. Stewart, Orvel Flowers, Melanie Cuellar, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Demonstration of the range over which the Langley Research Center digital computer charring ablation program (CHAP) can be used with confidence : comparisons of CHAP predictions and test data for three ablation materials / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1972]), by Carl B. Moyer, Kenneth A. Green, Langley Research Center, and Aerotherm Corporation (page images at HathiTrust)
• Environmental protection requirements for scout/shuttle auxiliary stages / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For Sale by the National Technical Information Service], 1980), by G. L. Qualls, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Effects of precursor heating on radiative and chemially reacting viscous flow around a Jovian entry body / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by S. N. Tiwari, Kuo-Yen Szema, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Investigation of char formation and surface recession of a composite ablation material with a silicone-resin base [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Allen G. McLain, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Heat-shield ablation measurements using radioisotope techniques / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1966]), by George W. Brandon and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Ablation performance of glasslike carbons, pyrolytic graphite, and artificial graphite in the stagnation pressure range 0.035 to 15 atmospheres / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1970]), by Howard G. Maahs and Langley Research Center (page images at HathiTrust)
• Afterbody heating data obtained from an atlas-boosted mercury configuration in a free body reentry / (Washington, D.C. : 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)
• Determination of kinetic parameters of six ablation polymers by thermogravimetric analysis / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1967]), by James B. Nelson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Methods for obtaining surface temperatures of materials in teh presence of extraneous radiation / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by B.L. Schilling and United States National Aeronautics and Space Administration (page images at HathiTrust)
• On chemical reactions in the char zone during ablation / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1971]), by Gary C. April, Eduardo Gonzalez Del Valle, Ralph W. Pike, Langley Research Center, and La.) Louisiana State University (Baton Rouge (page images at HathiTrust)
• Ablative heat shield design for space shuttle / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Rolf W. Seiferth, Langley Research Center, and Martin Marietta Denver Aerospace (page images at HathiTrust)
• Turbulent-skin-friction and heat-transfer charts adapted from the Spalding and Chi method / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Luther Neal, Mitchel H. Bertram, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Thermal cracking of phenolic-nylon pyrolysis products on passing through a heated char / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by George F. Sykes, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Graphite and ablative material response to CO₂-laser, carbon-arc, and xenon-arc radiation / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by William D. Brewer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Upwash patterns on ablating and nonablating cones at hypersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by John B. McDevitt, Jack A. Mellenthin, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A study of the effect of selected material properties on the ablation performance of artificial graphite. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1972), by Howard G. Maahs, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Shock-wave shapes and surface pressures on hemisphere- and cone-cylinders in low-density hypersonic flow including ablation / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Daryl J. Monson, Donald M. Kuehn, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Simulation of pyrolysis-gas flow through a char layer during ablation / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969]), by Ronald K. Clark and Langley Research Center (page images at HathiTrust)
• The lunar origin of tektites / (Washington, D.C. : National Aeronautics and Space Administration, 1963), by Dean R. Chapman, Howard K. Larson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Ablative performance of uncoated silicone-modified and shuttle baseline reinforced carbon composites / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Dennis L. Dicus, Ronald D. Brown, Russell N. Hopko, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Multidimensional gas flow through permeable char layers and its effects on ablation / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Harold G. Bush, Marvin B. Dow, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Analytical study of diffusion-controlled char oxidation and its effect on steady-state ablation of plastic materials / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by Gerald D. Walberg, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Measurement of optical radiation from the wake of ablating blunt bodies in flight at speeds up to 10 KM per second / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1965), by Jack D. Stephenson, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Effect on meteor flight of cooling by radiation and ablation / (Washington, D.C. : National Aeronautics and Space Administration, 1965), by H. Julian Allen, Nataline A. James, Barrett S. Baldwin, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Numerical analysis of the transient response of ablating axisymmetric bodies including the effects of shape change / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Stephen S. Tompkins, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Feasibility of standard evaluation procedures for ablating materials / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by Nevin K. Hiester and Carroll F. Clark (page images at HathiTrust; US access only)
• Thermophysical properties of a low-density phenolic-nylon ablation material / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by W. T. Engelke, C. D. Pears, and C. M. Pyron (page images at HathiTrust; US access only)
• A method for computing luminous efficiencies from meteor data / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by Barrett S. Baldwin, H. Julian Allen, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Analysis of the thermal response of high-density phenolic-nylon on a spacecraft launched by the Pacemaker vehicle system / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by William G. Witte, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Radiofrequency transmission characteristics of several ablation materials / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 2215], 1968), by Melvin C. Gilreath, Stark L. Castellow, William F. Croswell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Balance for measuring skin friction in the presence of ablation /, by James R. Bruno, Donald B. Risher, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• an Integral approach to transient heat-conduction problems with phase transition /, by Tse-Fou Zien and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• Instrumentation of aluminum bodies to determine interior temperature variations and rate of surface recession during exposure to nuclear explosions / ([Albuquerque, N.M.] : Sandia Corporation ; Washington, D.C. : Available from the Office of Technical Services, Department of Commerce, 1961), by Inc American Standard, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust; US access only)
• Boundary-layer transition experiments on pre-ablated graphite nosetips in a hyperballistics range /, by Daniel C Reda, Robert A. Leverance, and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• Investigation of ablation effects on hypersonic dynamic stability of a 10 cone /, by Dave R. Moore, Thomas C. Pope, Charles J. Stalmach, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor LTV Aerospace Corporation (page images at HathiTrust)
• Heat-transfer characteristics of blunt two-and three-dimensional bodies at supersonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, [1956]), by Glen Goodwin, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Ames Research Center (page images at HathiTrust)
• Results of ablation tests on several plastic models in a hypersonic wind tunnel /, by Constantino Economos, United States. Air Force. Air Research and Development Command. issuing agency, United States. Wright Air Development Center. sponsor, and sponsor Polytechnic Institute of Brooklyn (page images at HathiTrust)
• An ablation technique for enhancing reentry antenna performance; flight test results / (Hanscom AFB, Mass. : Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1974), by Dallas T. Hayes, J. Leon Poirier, John F. Lennon, Sheldon B. Herskovitz, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Determination of factors governing selection and application of materials for ablation cooling of hypervelocity vehicles /, by John H. Bonin, Donald E. Taylor, Channon F. Price, issuing body Wright Air Development Center, and sponsor United States. Air Force. Air Research and Development Command (page images at HathiTrust; US access only)
• Free-flight investigation of ablation effects n the stability of conical reentry configurations /, by C. J. Welsh, G. L. Winchenbach, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Force and pressure tests on cones with simulated ablated noses at Mach numbers 8 and 16 /, by J. S. Hahn, H. R. Little, Arnold Engineering Development Center. sponsor, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Research on the effects of collisions of small particles with bodies moving at hypersonic speed., by G. Whitnah, D. Rosenberg, W Torgeson, Arie Gaalswyk, J. Upton, G. Wehner, United States. Air Force. Air Research and Development Command. issuing body, Wright Air Development Center sponsor, and Inc. General Mills (page images at HathiTrust)
• Small vehicle dynamics study II : cross hatch studies /, by Charles O. White, Henry L. Moody, Richard M. Grabow, issuing body United States. Air Force. Systems Command, sponsor Space and Missile Systems Organization (U.S.), and sponsor Philco-Ford Corporation (page images at HathiTrust)
• Ablation and viscous effects on the force and moment characteristics of slender cone models at Mach 10 under laminar flow conditions /, by B. J. Griffith, B. M. Majors, W. T. Strike, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Finite difference schemes for the solution of the nosetip shape change equations /, by P. G. Crowell, issuing body United States. Air Force. Systems Command, sponsor Space and Missile Systems Organization (U.S.), and sponsor Aerospace Corporation (page images at HathiTrust)
• Optimization of a low heat load turbine inlet vane /, by Jamie J. Johnson, Ryan P. Lemaire, Michael J. Flanagan, John P. Clark, Paul I. King, United States. Air Force. Material Command. sponsor, and Ohio). |b Propulsion Directorate. issuing body Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)

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