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Wind tunnels -- Diffusers

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• Wind tunnels
• Diffusers

• Low-density hypervelocity wind tunnel diffuser performance (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), by M. W. Milligan, J. F. Bailey, Knoxville. Department of Mechanical and Aerospace Engineering niversity of Tennessee, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)

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

• Aerodynamic Design Guidelines and Computer Program for Estimation of Subsonic Wind Tunnel Performance (Washington: NASA, 1976), by William T. Eckert and Kenneth W. Mort (page images at HathiTrust)
• Wind Tunnels of NASA, by Donald D. Baals and William R. Corliss (illustrated HTML at NASA)
• NASA SC(2)-0714 Airfoil Data Corrected for Sidewall Boundary-Layer Effects in the Langley 0.3-Meter Transonic Cryogenic Tunnel (NASA technical paper 2890, 1989), by Renaldo V. Jenkins (page images at HathiTrust)
• Flight-Determined Aerodynamic Properties of a Jet-Augmented, Auxiliary-Flap, Direct-Lift-Control System Including Correlation With Wind-Tunnel Results (NASA Technical Note D-5128, corrected copy; Washington: National Aeronautics and Space Administration, 1969), by L. Stewart Rolls, Anthony M. Cook, and Robert C. Innis
  • PDF at NASA
  • page images at HathiTrust
• Experimental aerodynamics (Pitman publishing corporation, 1940), by Henry Christensen Pavian and Phillip Lincoln Michel (page images at HathiTrust)
• Smoke streams : visualized air flow (Coward-McCann, 1943), by Charles Townsend Ludington (page images at HathiTrust)
• Reports on wind tunnel experiments in aerodynamics (with five plates) (Smithsonian institution, 1916), by Edwin Bidwell Wilson, Charles Lee Brand, Donald W. Douglas, Henry Easter Rossell, Edgar Buckingham, Jerome Clarke Hunsaker, and Smithsonian Institution. Hodgkins fund (page images at HathiTrust)
• Wind-tunnel measurements of dispersion and turbulence in the wakes of nuclear reactor plants : final report, January 1975-December 1979 (The Commission :, 1980), by Robert N. Meroney, K. M. Kothari, J. A. Peterka, and U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research (page images at HathiTrust)
• An experimental and analytical investigation of the effect of truck-induced aerodynamic disturbances on passenger car control and performance - executive summary report. Interim report. (1971), by David H. Weir, R. F. Ringland, Robert K. Heffley, and Irving Louis Ashkenas (page images at HathiTrust)
• An experimental and analytical investigation of the effect of truck-induced aerodynamic disturbances on passenger car control and performance. Interim report. (1971), by David H. Weir, R. F. Ringland, Robert K. Heffley, and Irving Louis Ashkenas (page images at HathiTrust)
• Summary of staff and contract research on safety of wide buses. Summary report. (1973), by Terry L. Friesz, G. B. Pilkington, F. J. Daniels, D. W. Morrison, E. Kakaley, and D. F. Mela (page images at HathiTrust; US access only)
• A study of automotive aerodynamic drag. Final report. (1975), by J. E. Marte, R. W. Weaver, Donald W. Kurtz, and Bain Dayman (page images at HathiTrust)
• Influence of aerodynamic disturbances on vehicle handling (1978), by Richard H. Klein, Henry R. Jex, A. A. Blauvelt, and Irving Louis Ashkenas (page images at HathiTrust)
• Influence of aerodynamic disturbances on vehicle handling (1978), by Richard H. Klein, Irving Louis Ashkenas, and Henry R. Jex (page images at HathiTrust)
• Influence of aerodynamic disturbances on vehicle handling (1978), by Richard H. Klein, A. A. Blauvelt, and P. G. Van Valkenburgh (page images at HathiTrust)
• An experimental study of highway aerodynamic interferences. Final report. (1978), by D. P. Telionis, C. J. Fahrner, and G. S. Jones (page images at HathiTrust)
• Development of aerodynamic disturbance test procedures. Volume I: executive summary. Final report. (1979), by Richard H. Klein and Jeffrey R. Hogue (page images at HathiTrust)
• Development of aerodynamic disturbance test procedures. Volume II: technical report. Final report. (1979), by Richard H. Klein and Jeffrey R. Hogue (page images at HathiTrust)
• Aerodynamic characteristics of passenger vehicle/trailer combinations. Final report. (1982), by John W. Zellner (page images at HathiTrust)
• High-speed wind tunnels. (Headquarters Air Materiel Command, 1946), by Luigi Crocco (page images at HathiTrust; US access only)
• Axisymmetric Hall-arc jet wind tunnel driver study (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1967), by Robert Richter, Rolf D. Buhler, and Peter Lenn (page images at HathiTrust)
• The upwash correction for an oscillating wing in a wind tunnel. (Cornell Aeronautical Laboratory, Inc.], 1951), by Theodore R. Goodman (page images at HathiTrust)
• Characteristics of six research wind tunnels of the Ames Aeronautical Laboratory. (Washington, 1957), by United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Flow visualization by elastic light scattering in the boundary layer of a supersonic flow (National Aeronautics and Space Administration, Langley Research Center, 2000), by G. C. Herring, Mervin E. Hillard, and Langley Research Center (page images at HathiTrust)
• Investigation of ablation effects on hypersonic dynamic stability of a 10 cone (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), by Dave R. Moore, Thomas C. Pope, Charles J. Stalmach, Air Force Flight Dynamics Laboratory (U.S.), and LTV Aerospace Corporation (page images at HathiTrust)
• Aeronautical facilities catalogue (Washington, D.C. : Scientific and Technical Information Branch, National Aeronautics and Space Administration, 1985, 1985), by Frank E. Peñaranda, M. Shannon Freda, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Experimental evaluation of blockage ratio and plenum evacuation system flow effects on pressure distribution for bodies of revolution in 0.1-scale model test section of NASA Lewis Research Center's proposed altitude wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by Richard R. Burley, Douglas E. Harrington, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Detailed flow surveys of turning vanes designed for a 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by Royce D. Moore and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Experimental evaluation of turning vane designs for high-speed and coupled fan-drive corners of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by Thomas F. Gelder and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Experimental evaluation of honeycomb/screen configurations and short contraction section for NASA Lewis Research Center's altitude wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by Richard R. Burley, Douglas E. Harrington, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Evolution, calibration, and operational characteristics of the two-dimensional test section of the Langley 0.3-meter transonic cryogenic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by Charles L. Ladson, Edward J. Ray, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Finite-rate water condensation in combustion-heated wind tunnels (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by Wayne D. Erickson, Ramadas K. Prabhu, Gerald H. Mall, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Aerodynamic force measurements with a strain-gage balance in a cryogenic wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Richmond P. Boyden, Alice T. Ferris, William G. Johnson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Numerical study of the aerodynamic effects of using sulfur hexafluoride as a test gas in wind tunnels (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by W. Kyle Anderson and Langley Research Center (page images at HathiTrust)
• Computer program to improve Space Tracking and Data Acquisition Network station scheduling (National Aeronautics and Space Administration ;, 1966), by Walter D. Davis and Goddard Space Flight 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 (National Aeronautics and Space Administration ;, 1966), by John J. Bertin and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Laser-velocimeter surveys of merging vortices in a wind tunnel : complete data and analysis (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Victor R. Corsiglia, Kenneth L. Orloff, James D. Iversen, Iowa State University, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Transonic aerodynamic characteristics of a tailless fixed-wing supersonic transport model (National Aeronautics and Space Administration ;, 1966), by Edward J. Ray, Robert T. Taylor, and Langley Research Center (page images at HathiTrust)
• Application of two design methods for active flutter suppression and wind-tunnel test results (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Jerry R. Newsom, H. J. Dunn, Irving Abel, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Investigation of the asymmetric aerodynamic characteristics of cylindrical bodies of revolution with variations in nose geometry and rotational orientation at angles of attack to 58ånd Mach numbers to 2 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Robert L. Kruse, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Influence of free-stream disturbances on boundary-layer transition. (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Bill Harvey (page images at HathiTrust)
• Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F-15 airplane (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Lannie D. Webb, Stephen A. Whitmore, Dom Andriyich-Varda, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Aerodynamic design of the contoured wind-tunnel liner for the NASA supercritical, laminar-flow-control, swept-wing experiment (National Information Branch ;, 1984), by Perry A. Newman, John B. Peterson, E. Clay Anderson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Dynamic wind-tunnel tests of an aeromechanical gust-alleviation system using several different combinations of control surfaces (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Eric C. Stewart, Robert V. Doggett, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Thomas A. Byrdsong, Cuyler W. Brooks, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Experimental evaluation of wall Mach number distributions of the octagonal test section proposed for NASA Lewis Research Center's altitude wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Douglas E. Harrington, Robert R. Corban, Richard R. Burley, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Experimental evaluation of two turning vane designs for fan drive corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by Donald R. Boldman, Rickey J. Shyne, Royce D. Moore, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Dynamic measurement of total temperature, pressure, and velocity in the Langley 0.3-meter transonic cryogenic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Charles B. Johnson, P. Calvin Stainback, and Langley Research Center (page images at HathiTrust)
• Wake characteristics of an eight-leg tower for a mod-o type wind turbine : prepared for Dept. of Energy, Division of Solar Energy, Federal Wind Energy Program (Dept. of Energy, Division of Solar Energy ;, 1977), by Joseph M. Savino, Donald M. Sinclair, Lee H. Wagner, United States. Dept. of Energy. Division of Solar Energy, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Studies of condensation effects on airfoil testing in the Langley 0.3-meter transonic cryogenic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Robert M. Hall and Langley Research Center (page images at HathiTrust)
• Considerations for the installation of honeycomb and screeens to reduce wind-tunnel turbulence (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by James Scheiman, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel free-flight investigation of a model of a forward-swept-wing fighter configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Daniel G. Murri, Sue B. Grafton, Luat T. Nguyen, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Experiments in a three-dimensional adaptive-wall wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Edward T. Schairer and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Modifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by Charles D. Harris and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• The 13-inch magnetic suspension and balance system wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1989), by William G. Johnson and David A. Dress (page images at HathiTrust)
• A wind-tunnel study of the applicability of far-field sonic-boom theory to the space shuttle orbiter (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Harry W. Carlson, Robert J. Mack, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• An experimental investigation of end treatments for nonreturn wind tunnels (U.S. National Aeronautics and Space Administration ;, 1976), by William T. Eckert, J. E. Piazza, Kenneth W. Mort, United States National Aeronautics and Space Administration, U.S. Army Air Mobility Research and Development Laboratory, and Ames Research Center (page images at HathiTrust)
• A device for rapid determination of thermophysical properties of phase-change wind-tunnel models (National Aeronautics and Space Administration ;, 1976), by Theodore R. Creel and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A linearly controlled direct-current power source for high-current inductive loads in a magnetic suspension wind tunnel (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by John S. Tripp, Taumi S. Daniels, and Langley Research Center (page images at HathiTrust)
• Loads and performance data from a wind-tunnel test of model articulated helicopter rotors with two different blade torsional stiffnesses (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by William T. Yeager, Wayne R. Mantay, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Effect of jet exit vanes on flow pulsations in an open-jet wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by William L. Sellers and Langley Research Center (page images at HathiTrust)
• Computer program for calculating flow parameters and power requirements for cryogenic wind tunnels (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by David A. Dress and Langley Research Center (page images at HathiTrust)
• Evaluation of wind-tunnel gust response technique correlations with analytical and flight test results (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by L. Tracy Redd, Eleanor C. Wynne, Perry W. Hanson, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Evaluation of the Langley 4- by 7-meter tunnel for propeller noise measurements (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by P. J. W. Block, Garl L. Gentry, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Potential flow through a cascade of alternately displaced circular bodies : the rod-wall wind-tunnel boundary condition (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1984), by Joel L. Everhart and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Wind-tunnel investigation of an advanced general aviation canard configuration (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1984), by Joseph R. Chambers, Thomas M. Moul, Long P. Yip, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Description and calibration of the Langley Unitary Plan Wind Tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Charlie M. Jackson, William J. Monta, William A. Corlett, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Robert J. McGhee, William D. Beasley, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• The aerodynamic performance of several flow control devices for internal flow systems (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by William T. Eckert, Kenneth W. Mort, Brian M. Wettlaufer, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Space shuttle afterbody aerodynamics/plume simulation data summary (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Kenneth L. Blackwell, Leroy M. Hair, George C. Marshall Space Flight Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Onset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Robert M. Hall, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Longitudinal aerodynamic characteristics of an elliptical body with a horizontal tail at mach numbers 2.3 to 4.63 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Barrett L. Shrout, A. Warner Robins, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• A method for modifying two-dimensional adaptive wind-tunnel walls including analytical and experimental verification (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Joel L. Everhart and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Computer analysis of flow pertubations generated by placement of choke bumps in a wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Richard L. Campbell, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• The Langley 14- by 22-foot subsonic tunnel : description, flow characteristics, and guide for users (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Garl L. Gentry and Langley Research Center (page images at HathiTrust)
• Development of a distributed-parameter mathematical model for simulation of cryogenic wind tunnels (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by John S. Tripp and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• The effect of the converging flow field of a tandem-test-section on longitudinal stability measurements (National Aeronautics and Space Administration, 1968), by Shojiro Shindo and Robert G. Joppa (page images at HathiTrust; US access only)
• Full-scale wind tunnel tests of a low-wing, single-engine, light plane with positive and negative propeller thrust and up and down flap deflection (National Aeronautics and Space Administration, 1971), by Edward Seckel, United States National Aeronautics and Space Administration, Langley Research Center, and Princeton University (page images at HathiTrust)
• A wind tunnel investigation of panel response to boundary layer pressure fluctuations at mach 1.4 and mach 3.5 (National Aeronautics and Space Administration, 1966), by David Alan Bies (page images at HathiTrust; US access only)
• Wind-tunnel measurements in the wake of a simple structure in a simulated atmospheric flow (National Aeronautics and Space Administration, 1975), by A. C. Hansen, J. E. Cermak, J. A. Peterka, United States National Aeronautics and Space Administration, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Non-equilibrium Arc Tunnel Analysis : theory and analysis (National Aeronautics and Space Administration ;, 1975), by W. L. Bade, Jerrold M. Yos, Lyndon B. Johnson Space Center, and Avco Systems Division (page images at HathiTrust)
• Wind tunnel measurements in the wakes of structures (National Aeronautics and Space Administration ;, 1977), by H. G. C. Woo, J. E. Cermak, J. A. Peterka, George C. Marshall Space Flight Center, and Colorado State University (page images at HathiTrust)
• Calibration of transonic and supersonic wind tunnels (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by T. D. Reed, J. M. Cooksey, T. C. Pope, Vought Corporation, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Two dimensional aerodynamic interference effects on oscillating airfoils with flaps in ventilated subsonic wind tunnels (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Joseph Fromme, John Werth, Michael A. Golberg, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A method of calculating wind tunnel interference factors for tunnels of arbitrary cross-section (National Aeronautics and Space Administration, 1967), by Robert G. Joppa (page images at HathiTrust; US access only)
• Wind tunnel interference factors for high-lift wings in closed wind tunnels (National Aeronautics and Space Administration, 1973), by Robert G. Joppa, Langley Research Center, and University of Washington (page images at HathiTrust)
• F-15 rotary balance data for an angle-of-attack range of 8⁰ to 90⁰ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Billy Barnhart, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Mean velocity, turbulence intensity and turbulence convection velocity measurements for a convergent nozzle in a free jet wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by McColgan C J., R. S. Larsen, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Unsteady two dimensional airloads acting on oscillating thin airfoils in subsonic ventilated wind tunnels (National Aeronautics and Space Adiministration, Scientific and Technical Information Office ;, 1978), by Joseph Fromme, Michael Golberg, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Analysis of rotary balance data for the F-15 airplane including the effect of conformal fuel tanks (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Billy Barnhart, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Adaptive wall technology for minimization of wall interferences in transonic wind tunnels (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by Stephen W. D. Wolf and Langley Research Center (page images at HathiTrust)
• Sidewall boundary-layer measurements with upstream suction in the Langley 0.3-meter Transonic Cryogenic Tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by A. V. Murthy and Langley Research Center (page images at HathiTrust)
• Test sections for small theoretical wind-tunnel-boundary interference on V/STOL models (National Aeronautics and Space Administration, 1968), by Ray H. Wright, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theoretical study of the use of variable geometry in the design of minimal-correction V/STOL wind tunnels (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1969), by Harry H. Heyson, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• NASA TR R-364 (National Aeronautics and Space Administration ;, 1971), by Harry H. Heyson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TR R-300 (National Aeronautics and Space Administration ;, 1969), by George W. Jones, Robert W. Walker, Joseph J. Cincotta, George C. Marshall Space Flight Center, Martin Company, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Design study of test models of maneuvering aircraft configurations for the National Transonic Facility (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by S. A. Griffin, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and General Dynamics Corporation (page images at HathiTrust)
• Full-scale wind-tunnel test of the VZ-2 VTOL Airplane with particular reference to the wing stall phenomena (National Aeronautics and Space Administration, 1963), by Robert G. Mitchell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TR R-344 (National Aeronautics and Space Administration ;, 1970), by Ray H. Wright, James D. Keller, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Decomposition of nitric oxide in a hot nitrogen stream to synthesize air for hypersonic-wind-tunnel combustion testing (National Aeronautics and Space Administration ;, 1974), by John F. Zumdieck, Steven A. Zlatarich, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-2462 (National Aeronautics and Space Administration :, 1964), by George E. Sweet, Matthew M. Winston, Julian L. Jenkins, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust; US access only)
• Flight investigation of V/STOL height-control requirements for hovering and low-speed flight under visual conditions (National Aeronautics and Space Administration, 1967), by James R. Kelly, Perry L. Deal, John F. Garren, and Langley Research Center (page images at HathiTrust)
• Tables of interference factors for use in wind-tunnel and ground-effect calculations for VTOL-STOL aircraft. (National Aeronautics and Space Administration, 1962), by Harry H. Heyson (page images at HathiTrust; US access only)
• Static longitudinal stability of a rocket vehicle having a rear-facing step ahead of the stabilizing fins (National Aeronautics and Space Administration, 1961), by Robert J. Keynton, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Investigation of a mixed-compression axisymmetric inlet system at Mach numbers 0.6 to 3.5 (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by Donald B. Smeltzer and Norman E. Sorensen (page images at HathiTrust; US access only)
• NASA TN D-5857 (National Aeronautics and Space Administration ;, 1970), by James P. Shivers, George M. Ware, Marvin P. Fink, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5846 (National Aeronautics and Space Administration :, 1970), by Edward J. Hopkins, Virginia L. Sorensen, Don W. Jillie, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Wind-tunnel investigation of a jet transport airplane configuration with high thrust-weight ratio and an external-flow jet flap (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by Lysle P. Parlett, Charles Christian Smith, and Delma C. Freeman (page images at HathiTrust; US access only)
• Some anomalies observed in wind-tunnel tests of a blunt body at transonic and supersonic speeds (National Aeronautics and Space Administration ;, 1976), by Joseph D. Brooks, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• NASA TN D-6003 (National Aeronautics and Space Administration :, 1970), by Moses G. Farmer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5942 (National Aeronautics and Space Administration ;, 1970), by William A. Newsom, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5922 (National Aeronautics and Space Administration :, 1970), by Sanger M. Burk, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5893 (National Aeronautics and Space Administration ;, 1970), by Rodger L. Naeseth, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of very low blockage ratio boattail models in the Langley 16-foot transonic tunnel (National Aeronautics and Space Administration ;, 1976), by David E. Reubush and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel study of deflected-elevator flutter encountered on a T-Tail airplane (National Aeronautics and Space Administration, 1969), by Maynard C. Sandford, Charles L. Ruhlin, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel investigation of various small-scale rotor/wing configurations for VTOL composite aircraft in the cruise mode (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by James P. Shivers (page images at HathiTrust; US access only)
• NASA TN D-5901 (National Aeronautics and Space Administration :, 1970), by Charles G. Miller, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5903 (National Aeronautics and Space Administration :, 1970), by Joseph W. Cleary, Charles E. Duller, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Wind-tunnel investigation of the low-speed high-lift aerodynamics of a one-fifth scale variable-sweep supersonic transport (National Aeronautics and Space Administration, 1968), by Anthony M. Cook, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5338 (National Aeronautics and Space Administration ;, 1969), by Joseph F. Wasserbauer, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Exploratory wind-tunnel investigation of deployable flexible ventral fins for use as an emergency spin-recovery device (National Aeronautics and Space Administration, 1971), by Sanger M. Burk, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel investigation of an STOL aircraft configuration equipped with an external-flow jet flap (National Aeronautics and Space Administration :, 1969), by Lysle P. Parlett, James P. Shivers, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• NASA TN D-5600 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Lloyd S. Jernell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel investigation of V/STOL transport model with six wing-mounted lift fans (National Aeronautics and Space Administration, 1970), by William A. Newsom, Frederick L. Moore, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Free-flight and wind-tunnel studies of deployment of a dynamically and elastically scaled inflatable parawing model (National Aeronautics and Space Administration ;, 1968), by Alice T. Ferris, H. Neale Kelly, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5408 (National Aeronautics and Space Administration ;, 1969), by Delma C. Freeman, Richard D'Amato, Sue B. Grafton, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel study of slot spoilers for direct lift control (National Aeronautics and Space Administration, 1972), by Dominick Andrisani, Joseph W. Stickle, Garl L. Gentry, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• NASA TN D-6643 (National Aeronautics and Space Administration :, 1972), by William T. Suit, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of a mixed compression axisymmetric inlet at Mach number 5.3 (National Aeronautics and Space Administration, 1972), by Eldon A. Latham, Norman E. Sorenson, and Donald B. Smeltzer (page images at HathiTrust)
• Effect of trailing edge geometry and thickness on the performance of certain turbine stator blading. (National Aeronautics and Space Administration :, 1972), by Herman W. Prust, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6656 (National Aeronautics and Space Administration :, 1972), by Irving Abel, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Results of full-scale wind tunnel tests on the H.126 jet flap aircraft (National Aeronautics and Space Administration, 1969), by Anthony M. Cook, Dale G. Jones, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Transition Reynolds numbers of separated flows at supersonic speeds (National Aeronautics and Space Administration :, 1960), by Howard K. Larson, Stephen J. Keating, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental studies of hypersonic boundary-layer transition and effects of wind-tunnel disturbances (National Aeronautics and Space Administration ;, 1974), by P. Calvin Stainback and Langley Research Center (page images at HathiTrust)
• An exploratory wind-tunnel investigation of the wake effect of a panel tip-mounted fan-jet engine on the lift-induced vortex (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1970), by James C. Patterson, Stuart G. Flechner, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Subsonic and transonic pressure distributions around a bluff afterbody in the wake of a 120⁰ cone for various separation distances (National Aeronautics and Space Administration :, 1971), by James Wayne Sawyer, Charles F. Whitcomb, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Large-scale wind-tunnel investigation of a V/STOL transport model with wing-mounted lift fans and fuselage-mounted life-cruise engines for propulsion (National Aeronautics and Space Administration, 1967), by Jerry V. Kirk, Leo P. Hall, Brent K. Hodder, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• NASA TN D-5468 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Kenneth W. Mort, Michael D. Falarski, Army Aeronautical Research Laboratory, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Drag of a supercritical body of revolution in free flight at transonic speeds and comparison with wind-tunnel data (National Aeronautics and Space Administration ;, 1971), by J. W. Usry, John W. Wallace, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Full-scale wind-tunnel tests of a small unpowered jet aircraft with a T-Tail (National Aeronautics and Space Administration ;, 1971), by Paul T. Soderman, Thomas N. Aiken, U.S. Army Air Mobility Research and Development Laboratory, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6416 (National Aeronautics and Space Administration ;, 1971), by Harry H. Heyson, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Aerodynamic characteristics of a 55⁰ swept parawing with large-diameter leading edges (NASA :, 1964), by Delwin R. Croom, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• wind-tunnel investigation of longitudinal aerodynamic characteristics of three propeller-driven VTOL configurations in the transition speed range, including effects of ground proximity (National Aeronautics and Space Administration :, 1960), by Richard E. Kuhn, William C. Hayes, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed wind-tunnel investigation of a wingless jet VTOL transport model (National Aeronautics and Space Administration, 1959), by Marion O. McKinney and Langley Research Center (page images at HathiTrust)
• Effect of air contamination in a helium tunnel (National Aeronautics and Space Administration, 1960), by Arthur Henderson, Frank E. Swalley, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation of a deflected-slipstream cruise-fan V/STOL aircraft wing (National Aeronautics and Space Administration, 1967), by William A. Newsom and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel investigation of paraglider models at supersonic speeds (National Aeronautics and Space Administration, 1961), by Robert T. Taylor and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Large-scale wind-tunnel investigation of a model with an external jet-augmented flap (National Aeronautics and Space Administration, 1967), by Jerry V. Kirk, Kiyoshi Aoyagi, David H. Hickey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of camber and twist on the aerodynamic characteristics of parawings having nominal aspect ratios of 3 and 65 (NASA, 1963), by Edward C. Polhamus, Rodger L. Naeseth, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of groundboard height on the aerodynamic characteristics of a lifting circular cylinder using tangential blowing from surface slots for lift generation (National Aeronautics and Space Administration, 1961), by Vernard E. Lockwood, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• NASA TN D-4504 (National Aeronautics and Space Administration ;, 1968), by Robert C. Robinson, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel investigation of steady-state aerodynamics of a composite-lift VTOL aircraft model (National Aeronautics and Space Administration ;, 1969), by Matthew M. Winston, Robert J. Huston, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation of sonic-boom characteristics of two simple wing models at Mach numbers from 2.3 to 4.63 (National Aeronautics and Space Administration, 1971), by Davis S. Miller, Odell A. Morris, Harry W. Carlson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transport properties of N₂ gas at cryogenic temperatures (National Aeronautics and Space Administration ;, 1974), by Walter E. Pearson and Ames Research Center (page images at HathiTrust)
• Low-speed static wind-tunnel investigation of a half-span fuselage and variable-sweep pressure wing model (National Aeronautics and Space Administration, 1971), by John E. Lamar, L. Wayne McKinney, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Aerodynamic characteristics of parawings having equal-length leading edges and keel (NASA, 1963), by Rodger L. Naeseth, Thomas G. Gainer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel investigation of an external-flow jet-flap transport configuration having full-span triple-slotted flaps (National Aeronautics and Space Administration :, 1971), by Lysle P. Parlett, Langley Directorate, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Power calculations for isentropic compressions of cryogenic nitrogen (National Aeronautics and Space Administration ;, 1977), by Jerry B. Adcock, Marilyn E. Ogburn, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The Cryogenic wind-tunnel concept for high Reynolds number testing (National Aeronautics and Space Administration ;, 1974), by Robert A. Kilgore and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation of a four-engine externally blowing jet-flap STOL airplane model. (National Aeronautics and Space Administration; [for sale by the National Technical Information Service, Springfield, Va.], 1970), by Raymond D. Vogler, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Completed tabulation in the United States of tests of 24 airfoils at high Mach numbers (derived from interrupted work at Guidonia, Italy in the 1.31- by 1.74-foot high-speed tunnel) (Washington, 1946), by United States National Advisory Committee for Aeronautics and Antonio Ferri (page images at HathiTrust)
• Correction factors for wind tunnels of elliptic section with partly open and partly closed test section (NACA, 1951), by Friedrich Wilhelm Riegels and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NASA's Propulsion Systems Laboratory, No. 1 & 2 (Washington, DC : NASA History Program Office, 2012, 2012), by Robert S. Arrighi and United States. NASA History Division (page images at HathiTrust)
• A wind tunnel investigation of the Deer Isle-Sedgwick Bridge. Phase I. (U.S. Department of Transportation, Federal Highway Administration, Research, Development, and Technology ;, 1988), by Harold R. Bosch and United States. Federal Highway Administration. Structures Division (page images at HathiTrust)
• Rotary balance data for an F-15 model with fuel tanks for an angle-of-attack range of 8⁰ to 90⁰ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Billy Barnhart, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Full-scale wind-tunnel investigation of the low-speed static aerodynamic characteristics of a model of a reentry capsule (National Aeronautics and Space Administration, 1959), by William I. Scallion and Langley Research Center (page images at HathiTrust)
• Heat-transfer and pressure measurements on a concove-nose cylinder for a mach number range of 2.49 to 4.44 (National Aeronautics and Space Administration, 1959), by Jr. Stallings, Paige B. Burbank, and Langley Research Center (page images at HathiTrust)
• Characteristics of environmental test equipment at the Langley Research Center (National Aeronautics and Space Administration;, 1965), by Sherman A. Clevenson and Ian O. MacConochie (page images at HathiTrust)
• Characteristics of major active wind tunnels at the Langley Research Center (National Aeronautics and Space Administration ;, 1965), by William T. Schaefer and Langley Research Center (page images at HathiTrust)
• Investigation of axially symmetric and two-dimensional multinozzles for producing supersonic streams (National Advisory Committee for Aeronautics, 1952), by Eli Reshotko, Rudolph C. Haefeli, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Instrumentation of the ames supersonic free-flight wind tunnel (National Advisory Committee for Aeronautics, 1952), by Robert O. Briggs, Stanley F. Schmidt, William J. Kerwin, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
• Boundary-layer measurements on several porous materials with suction applied (National Advisory Committee for Aeronautics, 1952), by George B. McCullough, Bruno J. Gambucci, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
• Performance and windmilling drag characteristics (National Advisory Committee for Aeronautics, 1948), by William A. Fleming, Robert O. Jr Dietz, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Analysis of turbine performance and effect of tail-pipe design on engine performance (National Advisory Committee for Aeronautics, 1948), by Richard P. Krebs, Frederick C. Foshag, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
• Combustion-chamber performance (National Advisory Committee for Aeronautics, 1948), by Bemrose Boyd, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Analysis of turbine performance of 19B-8 engine (National Advisory Committee for Aeronautics, 1948), by Richard P. Krebs, Frank L. Suozzi, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Operational characteristics (National Advisory Committee for Aeronautics, 1948), by Richard L. Golladay, Stanley L. Gendler, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
• Performance and windmilling drag characteristics (National Advisory Committee for Aeronautics, 1948), by William A. Fleming, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
• Ramp floor vent-tube mounting (National Advisory Committee for Aeronautics, 1948), by Robert S. Ruggeri, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
• Analysis of compressor performance (National Advisory Committee for Aeronautics, 1948), by Robert O. Dietz, John K. Kuenzig, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Operational characteristics (National Advisory Committee for Aeronautics, 1948), by William A. Fleming, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Analysis of combustion-chamber performance (National Advisory Committee for Aeronautics, 1948), by Reece V. Hensley, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
• Air-flow and power characteristics of the Langley 16-foot transonic tunnel with slotted test section (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 (page images at HathiTrust)
• Preliminary investigation of shock-wave reflections in a small closed ballistic range with various types of walls (National Advisory Committee for Aeronautics, 1952), by Alexander Peter Sabol, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• An experimental investigation of the transonic-flow-generation and shock-wave-reflection characteristics of a two-dimensional wind tunnel with 17-percent-open perforated walls (National Advisory Committee for Aeronautics, 1954), by Don D. Davis, George M. Stokes, Thomas B. Sellers, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• The development of an 8-inch by 8-inch slotted tunnel for Mach numbers up to 1.28 (National Advisory Committee for Aeronautics, 1955), by B. H. Little, James M. Cubbage, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Spectrum of turbulence in a contracting stream (National Advisory Committee for Aeronautics, 1952), by Herbert Spencer Ribner, Maurice Tucker, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Some possibilities of using gas mixtures other than air in aerodynamic research (National Advisory Committee for Aeronautics, 1954), by Dean R. Chapman and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• The design of wind tunnels and wind tunnel propellers (G.P.O., 1919), by Edward P. Warner, C. M. Herbert, F. H. Norton, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• The Sandia dust tube : development and an experiment (Sandia Corporation, 1959), by John Robert Banister, Wade T. Parker, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust; US access only)
• Study of real gas and heat transfer effects on the design of hotshot wind tunnels (Sandia Corporation, Technical Information Division ;, 1960), by Jackson R. Stalder, David K. Eberly, Morris W. Rubesin, Inc Vidya, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
• AEDC test facilities handbook. (Arnold Engineering Development Center, Air Force, 1959), by Arnold Engineering Development Center (page images at HathiTrust)
• Wind tunnel supply headers (Aberdeen, Maryland : Aberdeen Proving Ground, 1970., 1970), by Anders S. Platou, U.S. Army Ballistic Research Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Charts for equiibrium flow properties of carbon dioxide in hypervelocity nozzles (Scientific and Technical Information Division, National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1965), by Leland H. Jorgensen and Robert J. Redmond (page images at HathiTrust)
• Evaluation of the T-755/GMQ-20 wind speed and direction transmitter (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1965., 1965), by Russell M. Peirce and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Upper atmosphere O-atom densities by wind tunnel simulation of nitric oxide releases (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1967., 1967), by D. Golomb, R. Earl Good, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Edmund T. Allen memorial aeronautical laboratories. (Boeing Aircraft Co., 1945), by Boeing Aircraft Company (page images at HathiTrust; US access only)
• Acquisition and utilization of wind tunnels by the National Aeronautics and Space Administration : report to the Committee on Science and Technology, House of Representatives (U.S. General Accounting Office, 1976), by United States General Accounting Office and United States. Congress. Senate. Committee on Science and Technology (page images at HathiTrust)
• Naval Ordnance Laboratory megawatt research arc (White Oak, Maryland : United States Naval Ordnance Laboratory, 1964., 1964), by Erhard M. Winkler, L.J. Milner, Richard L. Humphrey, R. E. Lee, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Wind tunnel free-flight testing techniques for planar motion employed at the Naval Ordnance Laboratory (White Oak, Maryland : United States Naval Ordnance Laboratory, 1967., 1967), by A Leonas, F. Regan, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Wind tunnel simulation of head-on bow wave-blast wave interactions (White Oak, Maryland : United States Naval Ordnance Laboratory, 1967., 1967), by David L. Merritt, P. M. Aronson, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• The prediction of errors and the improvement of data obtained in wind-tunnel heat-transfer tests (White Oak, Maryland : United States Naval Ordnance Laboratory, 1970., 1970), by Donald M. Wilson and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Concentration and flux of wind-blown snow (US Army Corps of Engineers, Cold Regions Research & Engineering Laboratory, 1986), by Malcolm Mellor, Gregor Fellers, and United States Army Corps of Engineers (page images at HathiTrust)
• Wind tunnel tests on airfoil boundary layer control using a backward-opening slot (National Advisory Committee for Aeronautics, 1931), by Millard J. Bamber and Langley Memorial Aeronautical Library (page images at HathiTrust)
• Perforated transonic wind tunnel walls (Providence, 1954), by P. F. Maeder (page images at HathiTrust; US access only)
• Low-drag bomb with freely spinning stabilizers (Silver Spring, Marlyand. : Naval Ordnance Laboratory, White Oak, 1973., 1973), by Frank J. Regan, J. F. Tanner, J. H. W. Shannon, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Measurements of a supersonic favorable-pressure-gradient turbulent boundary layer with heat Transfer : part 1 -data compilation. (Silver Spring, Maryland : Naval Ordnance Laboratory, 1973., 1973), by Robert L. P. Voisinet, Roland E. Lee, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Comparative measurements of total temperature in a supersonic turbulent boundary layer using a conical equilibrium and combined temperature-pressure probe. (Silver Spring, Maryland : Naval Ordnance Laboratory, 1974, 1974), by R. L. P. Voisinet, H. U. Meier, Roland E. Lee, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• NOL mach 18 hypervelocity research tunnel (Defense Technical Information Center, 1974), by Ray H. Cornett, Alton G Keel, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Influence of roughness on heat transfer and transition : ART Program Data Report. (Silver Spring, Maryland. : Naval Ordinance Laboratory, White Oak, 1973., 1973), by R. E. Phinney, F. P. Baltakis, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• NO-O chemiluminescent reaction in a low-density wind tunnel (L. G. Hansom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1966., 1966), by F. P. Delgreco, R. E. Good, R. A. Cassanova, Jan A. van der Bliek, D. Golomb, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Supersonic wind tunnel tests of ring-wing configurations (Wright-Patterson Air Force Base, Ohio, Wright Air Development Division, Air Research and Development Command., United States Air Force, 1958., 1958), by Leon H. Schindel, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
• The generation of gusts in a wind tunnel and measurement of unsteady lift on an airfoil (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1957., 1957), by L. C. Garby, J. D. Schetzer, A. M. Kuethe, United States. Air Force. Air Research and Development Command, University of Michigan, and Wright Air Development Center (page images at HathiTrust)
• Aerodynamic Deployable Decelerator Performance-Evaluation Program : Phase 2 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technical Division, Air Force Systems Command, United States Air Force, 1967., 1967), by E. Bloetscher, Air Force Flight Dynamics Laboratory (U.S.), and Goodyear Aerospace Corporation (page images at HathiTrust)
• An experimental study of the distribution of convective heat transfer to a large-scale model of parachute cloth (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), by E. R. G. Eckert, K. M. Krall, C. J. Scott, M. Ruiz-Urbieta, J. E. Anderson, Wright-Patterson Air Force Base (Ohio), University of Minnesota, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Pressure and heat transfer measurements for hypersonic flows over expansion corners and ahead of ramps (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1963), by Louis G. Kaufman, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command. Aeronautical Systems Division, and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Aerodynamic applications of plasma wind tunnels (Wright-Patterson Air Force Base, Ohio : Aeronautical Research Laboratory, Wright Air Development Division, Air Research and Development Command, United States Air Force, 1960., 1960), by Jackson R. Stalder, Boris Ragent, Charles E. Noble, Frederick K. Goodwin, United States. Air Force. Air Research and Development Command, and United States. Wright Air Development Center (page images at HathiTrust)
• Study of parachute scale effects (Wright-Patterson Air Force Base, Ohio : Flight Accessories Laboratory, Aeronautical Systems Division, Air Force Systems Command, 1963., 1963), by William B. Walcott, Technology Incorporated, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Use of strained coordinate perturbation method in transonic aeroelestic computations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), by P. Guruswamy, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Investigation of the flow field during the inflation of clustered parachutes (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), by R. J. Niccum, Nebojsa D. Kovacevic, University of Minnesota, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Pressure distribution in the wake of two bodies revolution at transonic and supersonic speeds (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by Helmut G. Heinrich, R. Sheldon Hess, University of Minnesota. Department of Aerospace Engineering and Mechanics, Wright-Patterson Air Force Base (Ohio), and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Design, calibration and simulation capability of the Rosemount aeronautical laboratories high temperature hypersonic facility (Wright-Patterson Air Force Base, Ohio : Aeronautical Research Laboratories, Air Force Research Division, Air Research and Development Command, United States Air Force, 1960., 1960), by Rudolph Hermann, United States. Air Force. Air Research and Development Command, United States. Wright Air Development Center, Aerospace Research Laboratories (U.S.), University of Minnesota, and Rosemount Aeronautical Laboratories (page images at HathiTrust)
• A theoretical analysis of a new type of heater for an intermittent hypersonic wind tunnel (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1957., 1957), by Antonio Ferri, Victor Zakkay, Paul A. Libby, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
• Preliminary experiments on the simulation of gusts in a wind tunnel (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research Development and Command, United States Air Force, 1955., 1955), by Arnold M. Kuethe, R. L. Roensch, L. C. Garby, J. D. Schetzer, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and University of Michigan. Department of Aeronautical Engineering (page images at HathiTrust)
• Infinite mass operating case (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1966., 1966), by H. D. Melzig, P. K. Schmidt, Deutsche Forschungsanstalt für Luft- und Raumfahrt (1961-1969), and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Advanced ejection seat for high dynamic pressure escape wind tunnel test report (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), by J. O. Bull, R. F. Yurczyk, D. T. Ther, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Boeing Military Airplane Company (page images at HathiTrust)
• Visualization of the flow field about parachute canopy models and approximation of canopy pressure distributions (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), by Charles A. Babish, Willard C. Hunter, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command. Research and Technology Division (page images at HathiTrust)
• Model study of the exhaust flow noise of the proposed AEDC high Reynolds number tunnel (Arnold Air Force Base, Tennessee : Von Karman Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), by J. E. Robertson, Wyle Laboratories, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Tests of a wind tunnel flutter model. Phase I, The critical flutter speed as a function of control surface dynamic balance and natural frequencies of vibration (Wright Field, Dayton, Ohio : War Department, Air Corps, Material Division, 1938., 1938), by Benjamin Smilg and United States. Army Air Forces. Air Matériel Command (page images at HathiTrust)
• Investigation of boundary-layer suction on a 20-caliber Ogive cylinder at Mach numbers 2.5, 3.0, 3.5, and 4.0 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1961., 1961), by W. T. Strike, S. Pate, Inc ARO, United States. Air Force. Air Research and Development Command, and Arnold Engineering Development Center (page images at HathiTrust)
• Boundary layer transition at supersonic speeds : three dimensional roughness effects (spheres) (Washington, D.C. : Air Force Office of Scientific Research, United States Air Force, 1961., 1961), by E. R. Van Driest, C. B. Blumer, United States. Air Force. Office of Scientific Research, and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
• Stability derivatives of a 10° cone executing planar and nonplanar motion at Mach 14 (Wright-Patterson Air Force Base, Ohio : Aerospace Research Laboratories, Hypersonic Research Laboratory, Air Force Systems Commany, 1974., 1974), by Kevin E. Yelmgren, Otto Walchner, Frank M. Sawyer, Aerospace Research Laboratories (U.S.), and Hypersonic Research Laboratory (U.S.) (page images at HathiTrust)
• Comparisons of free-flight and wind tunnel data on slender cones (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), by B. J. Griffith, Leo G. Siler, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Experimental heat transfer to blunt axisymmetric bodies near the limit of continuum flow (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1962., 1962), by J. Leith Potter, John T. Miller, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Wind tunnel investigation of a spike-bluff body combination for a monorail rocket sled M = 2.0 to M = 5.0 (Holloman Air Force Base, New Mexico : Air Force Office of Scientific Research, Directorate of Research Analyses, United States Air Force, 1962., 1962), by Rudolf Hermann, Donald Olson, Frederick Moynihan, United States. Air Force. Office of Scientific Research, Rosemount Aeronautical Laboratories, and University of Minnesota. Institute of Technology (page images at HathiTrust)
• Diffuser efficiency and flow process of supersonic wind tunnels with free jet test section. (United States Air Force, Air Material Command, Wright-Patterson Air Force Base, 1951), by Rudolf Hermann and United States. Air Force. Air Matériel Command (page images at HathiTrust; US access only)
• Laminar, transitional, and turbulent heat transfer to a cone-cylinder-flare body at Mach 8.0 (Air Force Office of Scientific Research, United States Air Force, 1962), by Victor Zakkay, Clifton J. Callahan, Polytechnic Institute of Brooklyn. Dept. of Aerospace Engineering and Applied Mechanics, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• F/A-18 forebody vortex control (National Aeronautics and Space Administration, Ames Research Center, 1994), by Brian R. Kramer and Ames Research Center (page images at HathiTrust)

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