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Air flow

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• Effect of turbulence on vortex-shedding air-velocity transducers / (Pittsburgh, Pa. : U.S. Dept. of the Interior, Bureau of Mines, 1985), by A. F. Cohen (page images at HathiTrust)
• Interim performance specifications for transducer modules used with the Bureau of Mines intrinsically safe mine monitoring system : carbon monoxide, methane, and air velocity / ([Washington, D.C.] : U.S. Dept. of the Interior, Bureau of Mines, [1983]), by J. E. Chilton and A. F. Cohen (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)
• Estimating airflow patterns over complex terrain / (Fort Collins, Colo. : U.S. Dept. of Agriculture, Forest Service, Rocky Mountain Forest and Range Experiment Station, 1976), by Michael A. Fosberg, Lawrence Krupnak, William E. Marlatt, and Colo.) Rocky Mountain Forest and Range Experiment Station (Fort Collins (page images at HathiTrust)
• KRISSY : user's guide to modeling three-dimensional wind flow in complex terrain / (Berkeley, CA : U.S. Dept. of Agriculture, Forest Service, Pacific Southwest Forest and Range Experiment Station, [1986]), by Michael A. Fosberg, M. L. Sestak, and Calif.) Pacific Southwest Forest and Range Experiment Station (Berkeley (page images at HathiTrust)
• Evaluation of an aeroelastic model technique for predicting airplane buffet loads [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1973), by Perry W. Hanson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Noise from interaction of flow with rigid surfaces : a review of current status of prediction techniques / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1972), by Richard E. Hayden, Langley Research Center, and Beranek Bolt (page images at HathiTrust)
• Large-scale static investigation of circulation-control-wing concepts applied to upper-surface-blowing aircraft / ([Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987), by M. D. Shovlin and Ames Research Center (page images at HathiTrust)
• A method of solution with tabulated results for the attached oblique shock-wave system for surfaces at various angles of attack, sweep, and dihedral in an equilibrium real gas including the atmosphere / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1960), by Robert L. Trimpi, Robert A. Jones, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental investigation of a 4 1/2-stage turbine with very high stage loading factor / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1973-1974), by D. C. Evans, Lewis Research Center, and General Electric Company (page images at HathiTrust)
• Influence of upstream flow discontinuities on the acoustic power radiated by a model air jet / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Colin G. Gordon, Gideon Maidanik, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Research on instabilities in atmospheric flow systems associated with clear air turbulence / (Washington, D.C. : National Aeronautics and Space Administration, [1970]), by James W. Clark, Paul G. Vogt, Richard C. Stoeffler, United States National Aeronautics and Space Administration, and United Aircraft Corporation (page images at HathiTrust)
• Program and charts for determining shock tube, expansion tube, and expansion tunnel flow quantities for real air / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Charles G. Miller, Sue E. Wilder, and Langley Research Center (page images at HathiTrust)
• Flow measurement in base cooling air passages of a rotating turbine blade / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Curt H. Liebert, Frank G. Pollack, and Lewis Research Center (page images at HathiTrust)
• The measurement of the flow of air in pipes by means of circular orifices in thin plates / (1907), by Alvin Charles Miller and Leroy Clark Ferry (page images at HathiTrust; US access only)
• Uniformity of air distribution in a lumber dry kiln / (Madison, Wis. : United States Dept. of Agriculture, Forest Service, Forest Products Laboratory, [1954]), by O. W. Torgeson, University of Wisconsin, and Forest Products Laboratory (U.S.) (page images at HathiTrust)
• Why the drying time of a kiln load of lumber is affected by air velocity / (Madison, Wis. : U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, [1954]), by O. W. Torgeson, University of Wisconsin, and Forest Products Laboratory (U.S.) (page images at HathiTrust)
• A contribution to the mathematical theory of air flow over mountains including effects of turbulent viscosity / (Los Angeles : Dept. of Meteorology, University of California, Los Angeles, 1962), by Berislav Makjanić (page images at HathiTrust)
• A mechanism for automatic and manual control of the air velocity at the window opening of fume hoods / (Oak Ridge, Tenn. : U.S. Atomic Energy Commission, Technical Information Division, 1948), by John Pitman Weber, U.S. Atomic Energy Commission, and Ames Laboratory (page images at HathiTrust)
• Air cleaning studies : progress report / (Boston, MA : Air Cleaning Laboratory - School of Public Health, Harvard University, 1952), by Edward M. Berly, Leslie Silverman, Melvin W. First, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Data book : physical properties and flow characteristics of air / (Cincinnati, Ohio : General Electric, Aircraft Nuclear Propulsion Dept., Reports and Publications Sub-Section, 1960), by J. L. Hobbs, Melvin E. Lapides, General Electric Company. Aircraft Nuclear Propulsion Department, U.S. Atomic Energy Commission, and General Electric Company (page images at HathiTrust)
• Documentation of AIR3D, an adaptation of the ground-water-flow code MODFLOW to simulate three-dimensional air flow in the unsaturated zone / (West Trenton, N.J. : U.S. Geological Survey ; Denver, CO : USGS, Earth Science Information Center, Open-File Reports Section, [distributor], 1995), by Craig J. Joss, Arthur L. Baehr, and Geological Survey (U.S.) (page images at HathiTrust)
• Analysis of the equations of airflow over mountains / ([Los Angeles, Calif.] : Dept. of Meteorology, University of California, Los Angeles, 1964), by Robert R. Long (page images at HathiTrust; US access only)
• An investigation at subsonic speeds of aerodynamic charactersitcs at angles of attack from -4⁰ to 100⁰ of a delta-wing reentry configuration having folding wingtip panels / (Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, 1960), by Bernard Spencer and Langley Research Center (page images at HathiTrust)
• The influence of directed air flow on combustion in a spark-ignition engine /, by A. M. Rothrock, Robert C. Spencer, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition / (Washington, D.C. : U.S. Government Printing Office, 1958), by Dean R. Chapman, Howard K. Larson, Donald M. Kuehn, and United States. National Advisory Committee for Aeronautics (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)
• A correspondence between normal-shock and blunt-body flows, (Buffalo, 1962), by Cornell Aeronautical Laboratory, Paul V. Marrone, and Walter E. Gibson (page images at HathiTrust)
• Investigation of a rapid-quench sampling probe for nonequilibrium air flows ([Arnold Air Force Station, Tenn., Arnold Engineering Development Center, Air Force Systems Command], 1967), by F. J. Stoddard and W. S. Watt (page images at HathiTrust)
• XB-70 compressor-noise reduction and propulsion-system performance for choked inlet flow / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 1970), by Terrill W. Putnam, Ronald H. Smith, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Outflow of a jet of compressed air into moving air. ([Dayton, Headquarters, Air Materiel Command, Wright-Patterson Air Force Base, 1949]), by M. Schaefer (page images at HathiTrust)
• A new method for providing continuous high-temperature air flow for hypersonic research, (Buffalo, N.Y., Cornell Aeronautical Laboratory, 1956), by Alexander H. Flax, William E. Smith, and Abraham Hertzberg (page images at HathiTrust)
• Theory of perturbations in stratified currents with applications to air flow over mountain barriers. (Chicago : Univ. of Chicago Press, [1947]), by Paul Queney (page images at HathiTrust; US access only)
• 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)
• Two-dimensional cold air cascade study of a film cooled turbine stator blade. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1975), by Herman W. Purst and Lewis Research Center (page images at HathiTrust)
• First derivatives of flow quantities behind two-dimensional, nonuniform supersonic flow over a convex corner / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by Christine M. Darden and Langley Research Center (page images at HathiTrust)
• Determination of corrections to flow direction sensor measurements over an angle-of-attack range from 0 ̊to 85 ̊/ (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by Thomas M. Moul and Langley Research Center (page images at HathiTrust)
• Second-order wave structure in supersonic flows / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by David A. Caughey, United States National Aeronautics and Space Administration, and Princeton University (page images at HathiTrust)
• Charts for equilibrium flow properties of air in hypervelocity nozzles / (Washington : National Aeronautics and Space Administration, [1962]), by Leland H. Jorgensen, Geyle M. Baum, and Ames Research Center (page images at HathiTrust)
• Measurements of flow properties in the vicinity of three wing-fuselage combinations at Mach numbers of 1.61 and 2.01 / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Harry W. Carlson and Langley Research Center (page images at HathiTrust)
• Distributed porous throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60 percent internal contraction / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by Robert J. Shaw, Bobby W. Sanders, Glenn A. Mitchell, and Lewis Research Center (page images at HathiTrust)
• Distributed educated throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by Robert J. Shaw, Bobby W. Sanders, Glenn A. Mitchell, and Lewis Research Center (page images at HathiTrust)
• Analysis of atmospheric flow over a surface protrusion using the turbulence kinetic energy equation with reference to aeronautical operating systems / (Washington : National Aeronautics and Space Administration, 1975), by Walter Frost and W. L. Harper (page images at HathiTrust)
• Turbulent atmospheric flow over a backward-facing step / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Upender Krishen Kaul, Walter Frost, University of Tennessee (Knoxville campus). Space Institute, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Atmospheric flow over two-dimensional bluff surface obstructions / (Washington : National Aeronautics and Space Administration, 1976), by Juergen Bitte, Walter Frost, George C. Marshall Space Flight Center, and University of Tennessee (Knoxville campus). Space Institute (page images at HathiTrust)
• A field study of air flow and turbulent features of advection fog / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by J. D. Connell, George C. Marshall Space Flight Center, University of Tennessee (System). Space Institute, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• A study of oxidation kinetics of nickel metal in flowing air and oxygen-nitrogen mixtures / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1964]), by Donald J. Progar, Beverley W. Lewis, and Langley Research Center (page images at HathiTrust)
• Growth due to buoyancy of weak homogeneous turbulence with shear / (Washington, D.C. : National Aeronautics and Space Administration, 1970), by Robert G. Deissler, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of nonequilibrium air streams in the Ames 1-foot shock tunnel [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by Robert Smith Hiers, John O. Reller, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Experimental investigation of air film cooling applied to an adiabatic wall by means of an axially discharging slot / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by S. Stephen Papell, Arthur M. Trout, and Lewis Research Center (page images at HathiTrust)
• Flow patterns and pressure distributions around a bluff afterbody in the wake of a 120° cone for various separation distances at Mach 3.0 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by William D. Deveikis, James Wayne Sawyer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Three-dimensional potential flow over hills and oval mounds / (Washington : National Aeronautics and Space Administration ;, 1976), by Robert Siegel and Lewis Research Center (page images at HathiTrust)
• Construction of a simple air flowmeter / ([Washington, D.C. : U.S. Department of Agriculture, Bureau of Entomology and Plant Quarantine, 1950]), by Robert A. Fulton, Frank S. Phinney, and United States. Bureau of Entomology and Plant Quarantine (page images at HathiTrust)
• Flow tables for air (₋ga₋s=1.4) passing an abrupt area increase oblique to the flow direction. (Wright-Patterson Air Force Base, Ohio, Aerospace Research Laboratories, Office of Aerospace Research, U.S. Air Force, 1964), by Arthur J. Wennerstrom (page images at HathiTrust)
• Performance trends of an air-cooled steam condenser under windy conditions : PIER final project report / ([Sacramento, Calif.] : California Energy Commission, [2008]), by Detlev G Kröger, J. A. van Rooyen, University of Stellenbosch. Institute for Thermodynamics and Mechanics, and California Energy Commission. Public Interest Energy Research (page images at HathiTrust)
• Discomfort due to wind near buildings : aerodynamic concepts / (Washington : Dept. of Commerce, National Bureau of Standards : For sale by the Supt. of Docs., U.S. Govt. Print. Off., 1978), by J. Gandemer, inc Information Simplified, Center for Building Technology, and Scientific and Technical Center for Architectural Engineering (page images at HathiTrust)
• A low-velocity airflow calibration and research facility / (Washington : Dept. of Commerce, Office of the Assistant Secretary of Commerce for Science and Technology, National Bureau of Standards : For sale by the Supt. of Docs., U.S. Govt. Print. Off., 1979), by L. P. Purtell, P. S. Klebanoff, United States. Bureau of Mines. Office of the Assistant Director--Mining, and Center for Mechanical Engineering and Process Technology (U.S.). Fluid Engineering Division (page images at HathiTrust)
• Wing-fuselage interference tail buffeting, and air flow about the tail of a low-wing monoplane / (Washington, D.C. : Government Printing Office, 1934), by James A. White, Manely J. Hood, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
• Performance of square-edged orifices and orifice-target combinations as air mixers / (Washington : 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)
• Flow and measurement of air and gases. (London, C. Griffin and company, limited, 1919), by Alec Birks 1887- Eason (page images at HathiTrust; US access only)
• Performance of louvered devices as air mixers / ([Washington] : 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)
• Smoke streams : visualized air flow / (New York : Coward-McCann, 1943), by Charles Townsend Ludington (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 /, by R. Eichhorn, A. D. Anderson, E. R. G. Eckert, United States. Air Force. Air Research and Development Command. sponsor, and Wright Air Development Center issuing body (page images at HathiTrust)
• On the flow over a finite wedge in the lower transonic region /, by Hideo Yoshihara, United States. Air Force. Air Research and Development Command. sponsor, and Wright Air Development Center issuing body (page images at HathiTrust)
• Symposium on parachute textiles /, by sponsor United States. Air Force. Air Research and Development Command and issuing body Wright Air Development Center, ed. by Joyce C. McGrath (page images at HathiTrust)
• Theoretical and experimental cascade flow investigations at high subsonic Mach numbers /, by U. Hopkes and issuing body United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Supersonic mixing of jets and turbulent boundary layers /, by Harry E. Bailey, Arnold M. Kuethe, United States. Air Force. Air Research and Development Command. sponsor, and Wright Air Development Center (page images at HathiTrust)
• Friction factors for metal mine airways /, by G. E. McElroy, A. S. Richardson, and United States Bureau of Mines (page images at HathiTrust)
• The Flow of air through circular orifices in thin plates / (Urbana, Ill. : University of Illinois, 1932), by Joseph Albert Polson and Joseph Gibson Lowther (page images at HathiTrust; US access only)
• Impact of using auxiliary fans on coal mine ventilation efficiency and cost / (Washington, D.C. : U.S. Dept. of the Interior, Bureau of Mines, 1990), by Fred N. Kissell, Dan J. Brunner, Malcolm J. McPherson, and Keith G. Wallace (page images at HathiTrust)
• A hot-wire anemometer for measuring air flow through engine radiators / (Washington, D.C. : U.S. Dept. of Commerce, Bureau of Standards : U.S. Govt. Print. Off., 1925), by Carl George Frederick Zobel, L. B. Carroll, and United States. National Bureau of Standards. Technologic Papers (page images at HathiTrust)
• A survey of methods for turbojet thrust measurement applicable to flight installation / (Washington, D.C. : National Advisory Committee for Aeronautics, [1955]), by William A. Fleming, David S. Gabriel, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Investigation of an asymmetric "penshape" exit having circular projections and discharging into quiescent air / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by James F. Connors, Rudolph C. Meyer, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• An inlet design concept to reduce flow distortion at angle of attack / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Carl F. Schueller, Leonard E. Stitt, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effects of aspect ratio on air flow at a high subsonic mach numbers / (Washington, D.C. : National Advisory Committee for Aeronautics, 1948), by W. F. Lindsey, Milton D. Humphreys, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Pressure measurements on a body of revolution in the Langley 16-foot transonic tunnel and a comparison with free-fall data / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Joseph M. Hallissy, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Studies of flow distribution in the core of a quarter-scale flow model of the PWR reactor / (Columbus, OH : Battelle Memorial Institute, [1956]), by Herbert R. Hazard, John M. Allen, U.S. Atomic Energy Commission, and Battelle Memorial Institute (page images at HathiTrust)
• Component performance investigation of J71 experimental turbine. (Washington, D.C. : National Advisory Committee for Aeronautics, 1956), by Donald A. Petrash, Elmer H. Davison, Harold J. Schum, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Preliminary investigation at low speeds of swept wings in rolling flow / (Washington, D.C. : National Advisory Committee for Aeronautics, 1947), by David Feigenbaum, Alex Goodman, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Note on the accuracy of a method for rapidly calculating the increments in velocity about an airfoil due to angle of attack / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by Laurence K. Loftin and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Approximate turbulent boundary-layer development in plane compressible flow along thermally insulated surfaces with application to supersonic-tunnel contour correction / (Washington, D.C. : National Advisory Committee for Aeronautics, 1950), by Maurice Tucker and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Calculation of compressible potential flow past slender bodies of revolution by an integral method / (Washington, D.C. : National Advisory Committee for Aeronautics, 1950), by Milton M. Klein, W. Perl, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Two-dimensional compressible flow in centrifugal compressors with logarithmic-spiral blades / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Gaylord O. Ellis, John D. Stanitz, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Extension of the theory of oscillating airfoils of finite span in subsonic compressible flow / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Eric Reissner and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Generalization of boundary-layer momentum-integral equations to three-dimensional flows including those of rotating system / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Artur Mager and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Transonic flow past a wedge profile with detached bow wave : general analytical method and final calculated results / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Walter G. Vincenti, Cleo B. Wagoner, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Flow through cascades in tandem / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by William E. Spraglin and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Experimental aerodynamic derivatives of a sinusoidally oscillating airfoil in two-dimensional flow / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Robert L. Halfman and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• An experimental investigation of transonic flow past two-dimensional wedge and circular-arc sections using a Mach-Zehnder interferometer / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Arthur E. Bryson and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• The normal component of the induced velocity in the vicinity of a lifting rotor and some examples of its application / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by Walter Castles, Jacob Henri De Leeuw, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• A visualization study of secondary flows in cascades / (Washington, D.C. : National Advisory Committee for Aeronautics, [1953]), by Arthur G. Hansen, George R. Costello, Howard Z. Herzig, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Comparison of secondary flows and boundary-layer accumulations in several turbine nozzles / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by Milton G. Kofskey, Howard Z. Herzig, Hubert W. Allen, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Design of two-dimensional channels with prescribed velocity distributions along the channel walls. (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by John D. Stanitz and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• An expansion of tables II and III of N.A.C.A. TN no. 1428., by U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
• Doppler radar investigation of flow patterns within thunderstorms / (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1974), by Michael J. Kraus and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Interim performance specifications for transducer modules used with the Bureau of Mines intrinsically safe mine monitoring system : carbon monoxide, methane, and air velocity / ([Washington, D.C.] : U.S. Dept. of the Interior, Bureau of Mines, 1983), by J. E. Chilton and A. F. Cohen (page images at HathiTrust)
• Effect of turbulence on vortex-shedding air-velocity transducers / (Washington, D.C. : U.S. Dept. of the Interior, Bureau of Mines, 1985), by A. F. Cohen (page images at HathiTrust)
• Correction factors for low-velocity airflow measurements in mines / ([Washington, D.C.] : Dept. of the Interior, Bureau of Mines, [1979]), by Edward D. Thimons, Fred N. Kissell, and S. D. Maksimovic (page images at HathiTrust)
• Flow of air and natural gas through porous media / (Washington, D.C. : U.S. Govt. Print. Off., Bureau of Mines, 1938), by Theodore W. Johnson and David Benjamin Taliaferro (page images at HathiTrust)
• Development of air distributor caps for a fluidized bed / ([Idaho Falls, Idaho] : U.S. Atomic Energy Commission, Idaho Operations Office, 1964), by J. C. Petrie, Idaho Chemical Processing Plant, Idaho National Reactor Testing Station, and Phillips Petroleum Company. Atomic Energy Division (page images at HathiTrust)
• Distribution of air in metal-mine ventilation with especial reference to flexible tubing methods / ([Washington, D.C.] : U.S. Dept. of the Interior, Bureau of Mines, 1923), by D. Harrington and United States Bureau of Mines (page images at HathiTrust)
• Theoretical and experimental investigation of the subsonic-flow fields beneath swept and unswept wings with tails of vortex-induced velocities / (Washington, D.C. : National Advisory Committee for Aeronautics, [1956]), by William J. Alford and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99. (Washington, D.C. : National Advisory Committee for Aeronautics, [1951]), by L. J. Obery, G. W. Englert, United States. National Advisory Committee for Aeronautics. NACA research memorandum, United States. National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Investigation of three types of supersonic diffuser over a range of Mach numbers from 1.75 to 2.74 / (Washington, D.C. : National Advisory Committee for Aeronautics, [1951]), by L. Eugene Baughman, Larence I. Gould, United States. National Advisory Committee for Aeronautics. NACA research memorandum, United States. National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Tests of a small-scale NACA submerged inlet at transonic Mach numbers / (Washington, D.C. : National Advisory Committee for Aeronautics, [1950]), by L. Stewart Rolls, George A. Rathert, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Heat transfer from high-temperature surfaces to fluids. (Washington, [D.C.] : National Advisory Committee for Aeronautics, [1949]), by Warren H. Lowdermilk, Milton D. Grele, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Heat transfer from high-temperature surfaces to fluids. (Washington, [D.C.] : National Advisory Committee for Aeronautics, [1948]), by Leroy V. Humble, Milton Grele, Warren H. Lowdermilk, United States. National Advisory Committee for Aeronautics. NACA research memorandum, United States. National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
• Preliminary attempts at isothermal compression of a supersonic air stream / (Washington, D.C. : National Advisory Committee for Aeronautics, [1956]), by E. Perchonok, F. Wilcox, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Investigation at supersonic and subsonic Mach numbers of auxiliary inlets supplying secondary air flow to ejector exhaust nozzles / (Washington, D.C. : National Advisory Committee for Aeronautics, [1956]), by Donald P. Hearth, Robert W. Cubbison, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Criteria for initial flow reversal in symmetrical twin-intake air-induction systems operating at supersonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, [1956]), by Andrew Beke, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Theoretical analysis of total-pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross-sectional areas/ (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Charles C. Graves, Jack S. Grobman, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Comparison of experimentally and analytically determined windmilling characteristics of a compressor with low over-all pressure ratio / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by James E. Hatch, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Air-flow surveys in the vicinity of representative NACA 1-series cowlings / (Washington, D.C. : National Advisory Committee for Aeronautics, 1948), by Robert W. Boswinkle, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Downwash, sidewash, and wave survey behind a 42⁰ sweptback wing at a Reynolds number of 6.8 x 10⁶ with and without a simulated ground / (Washington, D.C. : National Advisory Committee for Aeronautics, 1948), by G. Chester Furlong, Thomas V. Bollech, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Air-flow and power characteristics of the Langley 16-foot transonic tunnel with slotted test section / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Vernon G. Ward, Merwin D. Pearson, Charles F. Whitcomb, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• A theoretical and experimental study of wind-tunnel-wall effects on oscillating air forces for two-dimensional subsonic compressible flow / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by Harry L. Runyan, A. Gerald Rainey, Donald S. Woolston, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Effects of wing-body geometry on the lateral-flow angularities at subsonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1956), by Frank S. Malvestuto, William J. Alford, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Investigation of fixed-geometry supersonic inlets with bypass ducts for matching turbojet-engine air-flow requirements over a range of transonic and supersonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by Abraham Leiss, Walter J. Kouyoumjian, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Supplementary model studies of flow distribution in the core of the PWR reactor / (Columbus, OH : Battelle Memorial Institute, [1957]), by Lawrence J. Flanigan, Herbert R. Hazard, U.S. Atomic Energy Commission, and Battelle Memorial Institute (page images at HathiTrust)
• A variable-geometry annular cascade-type inlet at Mach numbers of 1.9 and 3.05 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1956), by James F. Connors, Rudolph C. Meyer, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Velocity distributions on symmetrical airfoils in closed tunnels by conformal mapping / (Washington, D.C. : National Advisory Committee for Aeronautics, 1948), by W. Perl, H. E. Moses, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• On the stability of the free laminar boundary layer between parallel streams / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by Martin Lessen and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Attainable circulation of airfoils in cascade / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by Arthur W. Goldstein, Artur Mager, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Theoretical relations between the stability derivatives of a wing in direct and in reverse supersonic flow / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by Sidney M. Harmon and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• On the theory of oscillating airfoils of finite span in subsonic compressible flow / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by Eric Reissner and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Investigation of turbulent flow in a two-dimensional channel / (Washington, D.C. : National Advisory Committee for Aeronautics, 1950), by John Laufer and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Analysis of turbulent free-convection boundary layer on flat plate / (Washington, D.C. : 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)
• Theoretical investigation of transonic similarity for bodies of revolution / (Washington, D.C. : National Advisory Committee for Aeronautics, 1950), by W. Perl, Milton M. Klein, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• On a source-sink method for the solution of the Prandtl-Busemann iteration equations in two-dimensional compressible flow / (Washington, D.C. : National Advisory Committee for Aeronautics, 1950), by Keith C. Harder, E. B. Klunker, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Similarity laws for transonic flow about wings of finite span / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by John R. Spreiter and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Correspondence flows for wings in linearized potential fields at subsonic and supersonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Sidney M. Harmon and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Two-dimensional transonic flow past airfoils / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Yung-Huai Kuo and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• A comparison of the experimental subsonic pressure distributions about several bodies of revolution with pressure distributions computed by means of the linearized theory / (Washington, D.C. : U.S. G.P.O., 1953), by Clarence W. Matthews and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Considerations on the effect of wind-tunnel walls on oscillating air forces for two-dimensional subsonic compressible flow / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Harry L. Runyan, Charles E. Watkins, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Spectrum of turbulence in a contracting stream / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Herbert Spencer Ribner, Maurice Tucker, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effect of Mach number on the flow and application of compressibility corrections in a two-dimensional subsonic-transonic compressor cascade having varied porous-wall suction at the blade tips / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by William B. Briggs and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Diffusion of heat from a line source in isotropic turbulence / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by M. S. Uberoi, Stanley Corrsin, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• One-dimensional analysis of choked-flow turbines / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Robert E. English, Richard H. Cavicchi, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Experimental investigation of loss in an annular cascade of turbine-nozzle blades of free vortex design / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by Hubert W. Allen, Richard E. Chamness, Milton G. Kofskey, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effect of variable viscosity and thermal conductivity on high-speed slip flow between concentric cylinders / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by T. C. Lin, R. E. Street, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Study of secondary-flow patterns in an annular cascade of turbine nozzle blades with vortex design / (Washington, D.C. : National Advisory Committee for Aeronautics, [1953]), by Harold E. Rohlik, Howard Z. Herzig, Hubert W. Allen, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• A study of hypersonic small-disturbance theory / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Milton Van Dyke and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Theoretical and experimental investigation of the effect of tunnel walls on the forces on an oscillating airfoil in two-dimensional subsonic compressible flow / (Washington, D.C. : National Advisory Committee for Aeronautics, 1955), by Harry L. Runyan, A. Gerald Rainey, Donald S. Woolston, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Simultaneous single element air temperature and velocity measurements / (Oak Ridge, Tenn. : United States Atomic Energy Commission, Technical Information Service, 1957), by James E. Benjamin, Ray W. Fahien, 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 / (Washington, D.C. : 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)
• Concerning the flow about ring-shaped cowlings. Part 8 - Further measurements on annular profiles / (Washington, D.C. : National Advisory Commitee for Aeronautics ;, [1952]), by Dietrich K©·uchemann, Johanna Weber, and United States. National Advisory Commitee for Aeronautics (page images at HathiTrust)
• Theoretical span load distributions and rolling moments for sideslipping wings of arbitrary plan form in incompressible flow / (Washington, D.C. : National Advisory Committee for Aeronautics, [1955]), by M. J. Queijo and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Air flow tests of a narrow collector passage with eight transverse feeder slots (applicable to 140E1 forward shield design studies) / (Cincinnati, Ohio : General Electric, Nuclear Materials and Propulsion Operation., 1961), by R. W. Bell, U.S. Atomic Energy Commission, and General Electric Company (page images at HathiTrust)
• Air cleaning studies : progress report, by Harvard University. Library of the Schools of Medicine and Public Health 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 / (Washington D.C. : National Advisory Committee for Aeronautics ;, 1946), by Frederick J. Hartwig 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 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by H. S. Mickley and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• The effect of increase in combustion-air inlet temperature from 80 to 130 degrees F on the sea-level performance of a 22-inch-diameter pulse-jet engine / (Washington, D.C. : National Advisory Committee for Aeronautics, [1946]), by Michael F. Valerino, Richard F. Hughes, Robert H. Essig, Aircraft Engine Research Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Air-flow and performance characteristics of engine-stage supercharger of a double-row radial aircraft engine. 2 - Effect of design variables / (Washington, D.C. : National Advisory Committee for Aeronautics, [1946]), by Edmund J. Baas, Paul D. Dugan, Aircraft Engine Research Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Doppler radar investigation of flow patterns within severe thunderstorms / (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1973), by Michael J. Kraus and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Measurement of recovery factors and friction coefficients for supersonic flow of air in a tube. [Part] II., by Joseph Kaye, Robert Howard Shoulberg, Tau-Yi Toong, Massachusetts Institute of Technology. Division of Industrial Cooperation, and United States. Office of Naval Research (page images at HathiTrust)
• Prediction of the pressure oscillations in cavities exposed to aerodynamic flow /, by D. L. Smith, L. L. Shaw, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Principles of air distribution. (New Britain, Conn. : Tuttle & Bailey, [1955]), by Richard D. Tutt (page images at HathiTrust; US access only)
• A study of flow phenomena in the wake of smokestacks. ([Menasha, Wis. : Printed by the George Banta publishing company, c1941]), by Robert Henry Sherlock and Edward Archibald Stalker (page images at HathiTrust)
• Heat transfer on an afterbody immersed in the separated wake of a hemisphere / (Washington, D.C. : National Advisory Committee for Aeronautics, [1958]), by Helmer V. Nielsen, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Ames Research Center (page images at HathiTrust)
• Approximate solutions for the flow about flat-top wing-body configurations at high supersonic airspeeds / (Washington, D.C. : National Advisory Committee for Aeronautics, [1958]), by Raymond C. Savin, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Ames Research Center (page images at HathiTrust)
• Viscous flow past a rotating translating blade with arbitrary velocity suction and slip (U) / (Albuquerque, New Mexico ; Sandia Corporation, 1963), by K. J. Touryan, Sandia Corporation, and U.S. Atomic Energy Commission (page images at HathiTrust; US access only)
• An investigation of the backflow phenomenon in centrifugal superchargers / (Washington, D.C. : National Advisory Committee for Aeronautics, [1945]), by William A. Benser, Jason J. Moses, Aircraft Engine Research Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Charge-air distribution among the cylinders of a double-row radial aircraft engine / (Washington, D.C. : National Advisory Committee for Aeronautics, [1946]), by Donald G. Guentert, John G. Ferkan, Aircraft Engine Research Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Tables and charts for the evaluation of profile drag from wake surveys at high subsonic speeds / (Washington, D.C. : National Advisory Committee for Aeronautics, [1945]), by Myron J. Block, S. Katzoff, Langley Aeronautical Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Collection and analysis of hinge-moment data on control-surface tabs / (Washington D.C. : National Advisory Committee for Aeronautics ;, 1947), by Paul E. Purser, Charles B. Cook, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Problem of slip flow in aerodynamics / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Robert E. Street and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• MGCR heat-exchanger test program interim report : isothermal air and helium tests / (Washington D.C., : Technical Services, Department of Commerce ;, 1959), by L. M. Casellini, H. C. Paulsen, General Dynamics Corporation. General Atomic Division, United States Maritime Administration, U.S. Atomic Energy Commission, and General Dynamics Corporation. Electric Boat Division (page images at HathiTrust)
• Mach tables for real gas equilibrium flow of air in hypervelocity test facilities with total temperatures to 10,000°K / (Albuquerque, New Mexico : Sandia Corporation, Technical Information Division ; Washington, D.C. : Available from the Office of Technical Services, Dept. of Commerce, [1961]), by Kennith L. Goin, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
• Flow over a slender body of revolution at supersonic velocities / (Washington D.C. : National Advisory Committee for Aeronautics ;, 1946), by Robert T. Jones, Kenneth Margolis, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Investigation of the penetration of an air jet directed perpendicularly to an air stream / (Washington, D.C. : National Advisory Committee for Aeronautics, 1948), by Edmund E. Callaghan, Robert S. Ruggeri, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• On the Second-order tunnel-wall-constriction corrections in two-dimensional compressible flow / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by E. B. Klunker, Keith C. Harder, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Airflow and precipitation trajectories within severe local storms which travel to the right of the winds /, by Keith A. Browning and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Measured air flow rates through microorifices and flow prediction capability /, by S. L Sutter, L. C Schwendiman, J Mishima, T. J Bander, and Fuel Cycle U.S. Nuclear Regulatory Commission. Division of Safeguards (page images at HathiTrust)
• Depleted uranium dioxide powder flow through very small openings /, by S. L Sutter, L. C. Schwendiman, P. C. Owzarski, J. Mishima, J. W. Johnston, Pacific Northwest Laboratory, Fuel Cycle U.S. Nuclear Regulatory Commission. Division of Safeguards, United States. National Technical Information Service, and United States Government Printing Office, ed. by G. B. Long (page images at HathiTrust)
• A review of some recent developments in hypersonic flow /, by Antonio Ferri, sponsor United States. Air Force. Air Research and Development Command, issuing body Wright Air Development Center, and sponsor Polytechnic Institute of Brooklyn (page images at HathiTrust)
• Weapon bay cavity noise environments, data correlation and prediction for the B-1 aircraft /, by A. G. Tipton, issuing agency Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Rockwell International (page images at HathiTrust)
• Research on sound propagation in sound-absorbent ducts with superimposed air streams : Volume 2 /, by F. Mechel, W. Schilz, and sponsor Aerospace Medical Research Laboratories (U.S.) (page images at HathiTrust)
• Research on sound propagation in sound-absorbent ducts with superimposed air streams : Volume 3 /, by F. Mechel, W. Schilz, P. Mertens, and sponsor Aerospace Medical Research Laboratories (U.S.) (page images at HathiTrust)
• Ionization nonequilibrium effects on the magnetogasdynamic interaction in the stagnation region of an axisymmetric blunt body /, by Donald Wayne Boyer, sponsor Cornell Aeronautical Laboratory, sponsor Wright-Patterson Air Force Base (Ohio), and sposor United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Air flow characteristics of parachute fabrics at simulated high altitudes /, by C. V. Seshadri, D. M Mellen, J. G. Krizik, S. Backer, G. A. Brown, issuing body Wright Air Development Center, and sponsor United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Investigation of the flow field during the inflation of clustered parachutes /, by R. J. Niccum, Nebojsa D. Kovacevic, sponsor University of Minnesota, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Cavity oscillation in cruise missile carrier aircraft /, by Harold W. Bartel, James M. McAvoy, issuing agency Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lockheed-Georgia Company (page images at HathiTrust)
• Research on sound propagation in sound-absorbent ducts with superimposed air streams : Volume 1 /, by F. Mechel and sponsor Aerospace Medical Research Laboratories (U.S.) (page images at HathiTrust)
• Axially symmetric mixing of two laminar incompressible streams : II. /, by T. Paul Torda, sponsor United States. Air Force. Air Research and Development Command, issuing body Wright Air Development Center, and sponsor University of Illinois (Urbana-Champaign campus). Aeronautical Engineering Department (page images at HathiTrust)
• Mechanical resistance in breathing systems : a theoretical analysis /, by Henry L. Bruns, sponsor United States. Air Force. Air Research and Development Command, and issuing body Wright Air Development Center (page images at HathiTrust)
• A review of the hypersonic research carried out at Princeton University from 1949-1955 /, by Seymour M. Bogdonoff, issuing body Wright Air Development Center, sponsor United States. Air Force. Air Research and Development Command, and sponsor Princeton University (page images at HathiTrust)
• Application of the ideal canopy flow concept to natural and artificial roughness elements. ([Ithaca, N.Y.], 1971), by Ronald Martin Cionco (page images at HathiTrust; US access only)
• The reversibility theorem for thin airfoils in subsonic and supersonic flow / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by Clinton E. Brown and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• The laminar boundary-layer flow on rotating cylinders. ([Ithaca, N.Y.], 1958), by Shao-Wen Liu (page images at HathiTrust; US access only)
• Experimental heat transfer to blunt axisymmetric bodies near the limit of continuum flow /, by J. Leith Potter, John T. Miller, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Experimental verification of the frictional pressure drop through porous media /, by Robert T. Crook, sponsor United States. Air Force. Systems Command. Aeronautical Systems Division, and issuing agency United States. Air Force. Systems Command (page images at HathiTrust)
• Pressure distribution tests of several sharp leading edge wings, bodies, and body-wing combinations at Mach 5 and 8 /, by R. E. Randall, J. L. Burk, D. R. Bell, Inc. sponsor ARO, United States. Air Force. Air Research and Development Command. sponsor, and Arnold Engineering Development Center. issuing body (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 /, by Thomas Woodrow Jackson, Harold L. Johnson, Calvin Oliver, Kenneth R. Purdy, issuing body Aerospace Research Laboratories (U.S.), and sponsor Georgia Institute of Technology (page images at HathiTrust)
• Supersonic flow past finite double wedge wings of variable thickness., by Maurice Holt, Bohyun Yim, issuing body United States. Air Force. Office of Scientific Research, and sponsor Brown University. Division of Applied Mathematics (page images at HathiTrust)
• Investigation of self-induced blowing and suction across a region of shock wave-boundary layer interaction /, by James R. Cooper, Robert H. Korkegi, and issuing body Aerospace Research Laboratories (U.S.) (page images at HathiTrust)
• Low-density stagnation-point heat transfer in hypersonic air flow /, by Charles F. Wittliff, Merle R. Wilson, issuing body Aerospace Research Laboratories (U.S.), and sponsor Cornell Aeronautical Laboratory (page images at HathiTrust)
• Supersonic flow past finite double wedge wings of variable thickness., by Maurice Holt, Bohyun Yim, issuing body United States. Air Force. Office of Scientific Research, and sponsor Brown University. Division of Applied Mathematics (page images at HathiTrust)
• On Three-dimensional swirling wakes /, by Martin H. Steiger, United States. Air Force. Office of Scientific Research. issuing body, and Polytechnic Institute of Brooklyn. Department of Aeronautical Engineering and Applied Mechanics. sponsor (page images at HathiTrust)

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