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Wind tunnels

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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
Static longitudinal and lateral stability and control characteristics of a right triangular pyramidal lifting reentry configuration at Mach numbers from 2.36 to 4.65 / (Washington, D.C. : National Aeronautics and Space Administration, 1963), by Nickolai Charczenko, C. Donald Babb, and Langley Research Center (page images at HathiTrust)
The wind-induced loads on a dynamically scaled model of a large missile in launching position / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Donald A. Buell, George C. Kenyon, and Ames 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 / (Washington, D.C. : 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 / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Jr. Stallings, Paige B. Burbank, and Langley Research Center (page images at HathiTrust)
Pressure data for four analytically defined arrow wings in supersonic flow / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by James C. Townsend, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Characteristics of environmental test equipment at the Langley Research Center, ([Washington, D.C.] National Aeronautics and Space Administration; Springfield, Va. for sale by the Clearinghouse for Federal Scientific and Technical Information, [1965]), by Sherman A. Clevenson and Ian O. MacConochie (page images at HathiTrust)
Characteristics of major active wind tunnels at the Langley Research Center / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1965), by William T. Schaefer and Langley Research Center (page images at HathiTrust)
Charts for equiibrium flow properties of carbon dioxide in hypervelocity nozzles, (Washington, 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)
Wind-tunnel investigation at mach numbers from 0.6 to 1.4 of several ejected pilot-seat models / (Washington : National Advisory Committee for Aeronautics, [1958]), by James L. Summers and Ames Research Center (page images at HathiTrust)
Description and initial calibration of the Langley hotshot tunnel with some real-gas charts for nitrogen / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Dept. of Commerce, Washington, D.C. 20230], 1963), by Fred M. Smith, Pierce L. Lawing, Edwin F. Harrison, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
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 / (Washington, D.C. : NACA, 1951), by Friedrich Wilhelm Riegels and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Investigation of the low-subsonic aerodynamic characteristics of a model of a modified lenticular reentry configuration / (Washington, D.C. : National Aeronautics and Space Administration, 1962), by George M. Ware and Langley Research Center (page images at HathiTrust)
Automatic control study of the icing research tunnel refrigeration system / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by Arthur W. Kieffer, Ronald H. Soeder, and Lewis Research Center (page images at HathiTrust)
Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8t̊o 90/̊ (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by William Mulcay, Julio Chu, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Low-speed investigation of the effects of wing sweep on the aerodynamic characteristics of parawings having equal-length leading edges and keel / (Washington [D.C.] : NASA, 1963), by Rodger L. Naeseth, Thomas G. Gainer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
The NATA code : theory and analysis / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1975), by W. L. Bade, Jerrold M. Yos, Lyndon B. Johnson Space Center, and Avco Systems Division (page images at HathiTrust)
Decomposition of nitric oxide in a hot nitrogen stream to synthesize air for hypersonic-wind-tunnel combustion testing / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by John F. Zumdieck, Steven A. Zlatarich, and Lewis Research Center (page images at HathiTrust)
Static longitudinal stability of a rocket vehicle having a rear-facing step ahead of the stabilizing fins / (Washington, [D.C.] : 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)
Results of full-scale wind tunnel tests on the H.126 jet flap aircraft / (Washington, D.C. : 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)
Experimental studies of hypersonic boundary-layer transition and effects of wind-tunnel disturbances / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by P. Calvin Stainback and Langley Research Center (page images at HathiTrust)
Test sections for small theoretical wind-tunnel-boundary interference on V/STOL models / (Washington, D.C. : 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)
A study of the simulation of flow with free-stream Mach number 1 in a choked wind tunnel / (Washington, DC : U.S. G.P.O., 1960), by John R. Spreiter, B. Jeanne Hyett, Donald W. Smith, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
Transport properties of N₂ gas at cryogenic temperatures / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Walter E. Pearson and Ames Research Center (page images at HathiTrust)
The Langley 14- by 22-foot subsonic tunnel : description, flow characteristics, and guide for users / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Garl L. Gentry and Langley Research Center (page images at HathiTrust)
Exploratory investigation of sound pressure level in the wake of an oscillating airfoil in the vicinity of stall / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1972), by Robin B. Gray, G. A. Pierce, Langley Research Center, and Georgia Institute of Technology (page images at HathiTrust)
A wind model for an elevated stol-port configuration / (Washington, D.C. : National Aeronautics and Space Administration, [1974]), by J. A. Peterka, J. E. Cermak, Ames Research Center, and Colorado State University (page images at HathiTrust)
Subsonic and transonic pressure distributions around a bluff afterbody in the wake of a 120⁰ cone for various separation distances / (Washington : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1971), by James Wayne Sawyer, Charles F. Whitcomb, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Drag of a supercritical body of revolution in free flight at transonic speeds and comparison with wind-tunnel data / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by J. W. Usry, John W. Wallace, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Numerical study of the aerodynamic effects of using sulfur hexafluoride as a test gas in wind tunnels / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by W. Kyle Anderson and Langley Research Center (page images at HathiTrust)
Visualization of leading edge vortices on a series of flat plate delta wings / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by Francis M. Payne, Robert C. Nelson, T. Terry Ng, Ames Research Center, and University of Notre Dame. Dept. of Aerospace and Mechanical Engineering (page images at HathiTrust)
Theoretical study of the use of variable geometry in the design of minimal-correction V/STOL wind tunnels / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1969), by Harry H. Heyson, 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 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : Clearinghouse for Federal Scientific and Technical Information, 1968), by Alice T. Ferris, H. Neale Kelly, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
A simplified holographic-interferometry technique for real-time flow visualization and analysis / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Sheila Ann T. Long, Don M. Robinson, Robert C. Spencer, and Langley Research Center (page images at HathiTrust)
Effects of canopy shape on low-speed aerodynamic characteristics of a 55⁰ swept parawing with large-diameter leading edges / (Washington, D.C. : NASA : For sale by the Office of Technical Services, Dept. of Commerce, 1964), by Delwin R. Croom, Langley Research Center, and United States National Aeronautics and Space Administration (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)
Full-scale wind-tunnel test of the VZ-2 VTOL Airplane with particular reference to the wing stall phenomena (Washington, D.C., National Aeronautics and Space Administration, 1963), by Robert G. Mitchell and United States National Aeronautics and Space Administration (page images at HathiTrust)
Investigation of a mixed compression axisymmetric inlet at Mach number 5.3 / (Washington, DC : National Aeronautics and Space Administration, 1972), by Eldon A. Latham, Norman E. Sorenson, and Donald B. Smeltzer (page images at HathiTrust)
The Cryogenic wind-tunnel concept for high Reynolds number testing / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Robert A. Kilgore and Langley Research Center (page images at HathiTrust)
Wind-tunnel investigation of paraglider models at supersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Robert T. Taylor and United States National Aeronautics and Space Administration (page images at HathiTrust)
Experimental and theoretical studies of the effects of camber and twist on the aerodynamic characteristics of parawings having normal aspect ratios of 3 and 6 / (Washington [D.C.] : 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 / (Washington, [D.C.] : 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)
Exploratory wind-tunnel investigation of deployable flexible ventral fins for use as an emergency spin-recovery device / (Washington, D.C. : 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)
Rotary balance data for an F-15 model with fuel tanks for an angle-of-attack range of 8⁰ to 90⁰ / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Billy Barnhart, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
Apollo wind tunnel testing program : historical development of general configurations / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966), by William C. Moseley, Joseph C. Martino, Manned Spacecraft Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
A swept wing panel in a low speed flexible walled test section / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987), by M. J. Goodyer and Langley Research Center (page images at HathiTrust)
Concentration and flux of wind-blown snow / ([Hanover, N.H.] : 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)
An exploratory wind-tunnel investigation of the wake effect of a panel tip-mounted fan-jet engine on the lift-induced vortex / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1970), by James C. Patterson, Stuart G. Flechner, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
NACA transonic wind-tunnel test sections / (Washington, D.C. : U.S. Government Printing Office, 1955), by Ray H. Wright, Vernon G. Ward, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Acquisition and utilization of wind tunnels by the National Aeronautics and Space Administration : report to the Committee on Science and Technology, House of Representatives / ([Washington] : 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)
Edmund T. Allen memorial aeronautical laboratories. ([Seattle : Boeing Aircraft Co., 1945]), by Boeing Aircraft Company (page images at HathiTrust; US access only)
Cryogenic wind tunnel models; design and fabrication : proceedings of a workshop held at NASA Langley Research Center, Hampton, Virginia, May 5-9, 1982 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Blair B. Gloss, Clarence P. Young, Langley Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Cryogenic Wind Tunnel Models Workshop (1982 : NASA Langley Research Center) (page images at HathiTrust)
Flow visualization and laser velocimetry for wind tunnels : proceedings of a NASA workshop held at Langley Research Center, Hampton, Virginia, March 25-26, 1982 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Jerome T. Foughner, William W. Hunter, Langley Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Workshop on Flow Visualization and Laser Velocimetry for Wind Tunnels (1982 : Langley Research Center) (page images at HathiTrust)
Preliminary investigation of the characteristics of a two-dimensional wing and propeller with the propeller plane of rotation in the wing-chord plane / (Washington : National Advisory Committee for Aeronautics, [1957]), by David H. Hickey, United States. National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
Micrometeorological wind tunnel facility : description and characteristics / (Fort Collins, Colo. : Fluid Dynamics and Diffusion Laboratory, Colorado State University, [1963]), by Erich J. Plate, J. E. Cermak, and Colorado State University. Fluid Dynamics and Diffusion Laboratory (page images at HathiTrust; US access only)
Large-scale wind-tunnel tests of a jet-transport-type model with leading- and trailing-edge high-lift devices / (Washington : National Advisory Committee for Aeronautics, [1958]), by David H. Hickey, Kiyoshi Aoyagi, and Ames Research Center (page images at HathiTrust)
Wind tunnel tests on airfoil boundary layer control using a backward-opening slot / (Washington, D.C. : National Advisory Committee for Aeronautics, 1931), by Millard J. Bamber and Langley Memorial Aeronautical Library (page images at HathiTrust)
The N.A.C.A. variable-density wind tunnel / (Washington, D.C. : Government Printing Office, 1932), by Eastman N. Jacobs, Ira H. Abbott, and United States. National Advisory Committee for Aeronautics (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 / (Washington, D.C. : 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)
Experimental investigation of wind-tunnel interference on the downwash behind an airfoil / (Washington, D.C. : National Advisory Committee for Aeronautics, 1937), by Abe Silverstein, S. Katzoff, and Langley Aeronautical Laboratory (page images at HathiTrust)
Development of an apparatus for wind tunnel dynamic experiments at high-[alpha] / ([Stanford, Calif.] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center : Joint Institute for Aeronautics and Acoustics, Stanford University, [1997]), by Nelson Pedreiro and Joint Institute for Aeronautics and Acoustics (page images at HathiTrust)
Wind-tunnel research comparing lateral control devices particularly at high angles of attack. ordinary ailerons rigged up 10 ̊when neutral / (Washington, D.C. : Government Printing Office, 1932), by Fred E. Weick, Carl J. Wenzinger, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
Axisymmetric Hall-arc jet wind tunnel driver study ([Wright-Patterson Air Force Base, Ohio, 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. ([Buffalo, 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)
High-speed wind tunnels. (Wright Field, Dayton, Ohio, Headquarters Air Materiel Command, [1946?]), by Luigi Crocco (page images at HathiTrust; US access only)
A theoretical investigation of simulation in expansion tubes and tunnels / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by Robert L. Trimpi, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
A wind-tunnel investigation of helicopter directional control in rearward flight in ground effect / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by Robert J. Huston, Charles E. K. Morris, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Investigation of a mixed-compression axisymmetric inlet system at Mach numbers 0.6 to 3.5, (Washington, 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)
Full-scale wind-tunnel investigation of the static longitudinal and lateral characteristics of a light single-engine low-wing airplane / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 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)
Charts for estimating boundary-layer transition on flat plates / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 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)
Large-scale wind-tunnel tests of an airplane model with four propellers and rotating cylinder flaps / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by James A. Weiberg, Stanley O. Dickinson, 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, (Washington, 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)
Wind-tunnel investigation of the aerodynamic pressures on the Apollo launch escape vehicle configuration / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by William C. Moseley, B. J. Wells, Manned Spacecraft Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
General theory of wall interference for static stability tests in closed rectangular test sections and in ground effect / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Harry H. Heyson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Aerodynamic forces on a stationary and oscillating circular cylinder at high Reynolds numbers / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 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)
Wind-tunnel lift interference on sweptback wings in rectangular test sections with slotted side walls / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 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)
Wind-tunnel investigation of various small-scale rotor/wing configurations for VTOL composite aircraft in the cruise mode, (Washington, 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)
Langley hotshot tunnel operations with helium at Mach numbers in excess of 30 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Charles G. Miller, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Performance testing of a main rotor system for a utility helicopter at 1/4 scale / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor, 1982]), by John D. Berry, Army Research and Technology Laboratories (U.S.). Structures Laboratory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Noise measurement in wind tunnels : workshop summary / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1982), by David H. Hickey, John Williams, Ames Research Center, and Workshop on Aeroacoustics Tunnel Testing Techniques (1979 : Ames Research Center) (page images at HathiTrust)
Aeronautical facilities catalogue / (Washington, DC : Scientific and Technical Information Branch, National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Supt. of Docs., U.S. G.P.O.], 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)
Space shuttle afterbody aerodynamics/plume simulation data summary / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1978), by 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 / (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 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Comparison of analytical and wind-tunnel results for flutter and gust response of a transport wing with active controls / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Irving Abel, Jerry R. Newsom, Boyd Perry, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
Studies of sidewall boundary layer in the Langley 0.3-Meter Transonic Cryogenic Tunnel with and without suction / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by A. V. Murthy, 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 / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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 / (Washington : National Aeronautics and Space Adiministration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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)
Effect of several tail configurations on the stability characteristics of a midwing supersonic-bomber model at mach numbers of 1.60, 1.90, 2.20, and 2.50 / (Washington, D.C. : National Aeronautics and Space Administration, 1960), by R. Franklin Wells, H. Norman Silvers, and Langley Research Center (page images at HathiTrust)
Stability and control characteristics at a mach number of 1.89 of a lightweight glider reentry configuration / (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Ross B. Robinson, M. Leroy Spearman, and Langley Research Center (page images at HathiTrust)
Applications and requirements for real-time simulators in ground-test facilities / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Dale J. Arpasi, Richard A. Blech, and Lewis Research Center (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 / ([Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / ([Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / ([Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / ([Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Finite-rate water condensation in combustion-heated wind tunnels / (Washington, D.C. : 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)
A computer program to improve STADAN station scheduling / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 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 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1966), by John J. Bertin and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
Laser-velocimeter surveys of merging vortices in a wind tunnel : complete data and analysis / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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)
Instrument error analysis as it applies to wind-tunnel testing / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by Emanuel Rind, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
Dynamic stability derivatives of space shuttle orbiter from wind-tunnel and approach and landing flight tests / (Washington, D.C. : National Aeronautics and Space Administration , Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Delma C. Freeman, Langley 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 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1966), by Edward J. Ray, Robert T. Taylor, and Langley Research Center (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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by 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. (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Bill Harvey (page images at HathiTrust)
Cryogenic wind tunnels : a selected, annotated bibliography / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Marie H. Tuttle, Robert A. Kilgore, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
Dynamic wind-tunnel tests of an aeromechanical gust-alleviation system using several different combinations of control surfaces / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National 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)
Cryogenic wind tunnels : a comprehensive, annotated bibliography / (Washington, DC : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991), by Marie H. Tuttle, Deborah L. Moore, Robert A. Kilgore, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by 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 / ([Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. For sale by the National Technical Information Service], 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 / ([Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Wind-tunnel test of an articlulated helicopter rotor model with several tip shapes / (Washington, D.C. : National Aeronautics and Space Administrat ion, Scientific and Technical Information Branch ; [Springfield, Va. : Fo r sale by the National Technical Information Service], 1980), by John D. Berry, Raymond E. Mineck, Army Research and Technology Laboratories (U.S.). Structures Laboratory, United States. Army Aviation Research and Development Command, 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Charles B. Johnson, P. Calvin Stainback, and Langley Research Center (page images at HathiTrust)
Magnetic suspension and balance systems : a selective annotated bibliography / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1980), by Marie H. Tuttle, Richmond P. Boyden, Robert A. Kilgore, and Langley Research Center (page images at HathiTrust)
Acoustic treatment of the NASA Langley 4- by 7-meter tunnel : a feasibility study / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by James C. Yu, A. Louis Abrahamson, 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 / (Washington : Dept. of Energy, Division of Solar Energy ; Springfield, Va. : Available through the National Technical Information Service, 1978), 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service,), 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service, 1981]), by James Scheiman, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
Flow visualization studies of a general research fighter model employing a strake-wing concept at subsonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by James M. Luckring, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Wind-tunnel free-flight investigation of a model of a forward-swept-wing fighter configuration / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Edward T. Schairer and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Milton Lamb, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Wind-tunnel investigation of a simulated gunship helicopter engine-exhaust-windstream interaction / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by John C. Wilson, Raymond E. Mineck, and Langley Research Center (page images at HathiTrust)
The 13-inch magnetic suspension and balance system wind tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by William G. Johnson and David A. Dress (page images at HathiTrust)
Effect of collector configuration on test section turbulence levels in an open-jet wind tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by G. S. Manuel, P. S. Barna, John K. Molloy, and Langley Research Center (page images at HathiTrust)
Flow improvements in the circuit of the Langley 4- by 7-meter tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Zachary T. Applin and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Flow visualization in a cryogenic wind tunnel using holography / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Alpheus W. Burner, William K. Goad, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
Wind-tunnel pressure data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊ / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Emma Jean Landrum and United States National Aeronautics and Space Administration (page images at HathiTrust)
Two dimensional transonic testing with splitter plates / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Sanford Davis, Bodapati Satyanarayana, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
A wind-tunnel study of the applicability of far-field sonic-boom theory to the space shuttle orbiter / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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 / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 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)
Loads and performance data from a wind-tunnel test of model articulated helicopter rotors with two different blade torsional stiffnesses / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by William T. Yeager, Wayne R. Mantay, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Improvement in the quality of flow visualization in the Langley 0.3-meter transonic cryogenic tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by W. L. Snow, William K. Goad, Alpheus W. Burner, and Langley Research Center (page images at HathiTrust)
Effect of jet exit vanes on flow pulsations in an open-jet wind tunnel / (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 William L. Sellers and Langley Research Center (page images at HathiTrust)
Computer program for calculating flow parameters and power requirements for cryogenic wind tunnels / (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 David A. Dress and Langley Research Center (page images at HathiTrust)
Adaptive wall wind tunnels : a selected, annotated bibliography / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Marie H. Tuttle, Raymond E. Mineck, and Langley Research Center (page images at HathiTrust)
Mass spectrometric gas composition measurements associated with jet interaction tests in a high-enthalpy wind tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Beverley W. Lewis and Langley Research Center (page images at HathiTrust)
Cryogenic wind tunnels : a selected, annotated bibliography / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985), by Marie H. Tuttle, Peggy D. McGuire, Robert A. Kilgore, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Results of buffet tests in a cryogenic wind tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Richmond P. Boyden, William G. Johnson, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Adaptive wall wind tunnels : a selected, annotated bibliography / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Marie H. Tuttle, Elizabeth B. Plentovich, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Background noise measurements from jet exit vanes designed to reduce flow pulsations in an open-jet wind tunnel / (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 Danny R. Hoad, R. M. Martin, United States. Army Aviation Systems Command. Structures Laboratory, and Langley Research Center (page images at HathiTrust)
Vapor-screen technique for flow visualization in the Langley Unitary Plan Wind Tunnel / (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 Odell A. Morris and Langley Research Center (page images at HathiTrust)
Evaluation of the Langley 4- by 7-meter tunnel for propeller noise measurements / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Similitude requirements and scaling relationships as applied to model testing / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by Chester H. Wolowicz, William P. Gilbert, James S. Bowman, Langley Research Center, Hugh L. Dryden Flight Research Center, 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Effects of vortex flaps on the low-speed aerodynamic characteristics of an arrow wing / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Long P. Yip, Daniel G. Murri, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service, 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)
Crossflow effects on steady and fluctuating pressures on an ogive-cylinder cone-frustum model in supersonic separated flow / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Jules B. Dods, Charles F. Coe, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Ames Research Center (page images at HathiTrust)
Force and moment flow-visualization, and boundary-layer tests on a Shuttle Orbiter model at Mach 6 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Robert L. Calloway, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests / ([Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Delma C. Freeman, Bernard Spencer, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
A method for modifying two-dimensional adaptive wind-tunnel walls including analytical and experimental verification / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
A theory for predicting boundary impedance and resonance, frequencies of slotted-wall wind tunnels, including plenum effects / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Raymond L. Barger, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
Development of a distributed-parameter mathematical model for simulation of cryogenic wind tunnels / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by John S. Tripp and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Wind-tunnel investigation of leading-edge thrust on arrow wings in supersonic flow / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Robert J. Mack and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Subsonic sphere drag measurements at intermediate Reynolds numbers / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by Kenneth R. Sivier, J. A. Nicholls, University of Michigan. Dept. of Aerospace Engineering, and Lewis Research Center (page images at HathiTrust)
Wind-tunnel measurements in the wake of a simple structure in a simulated atmospheric flow / (Washington, D.C. : 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)
Development of an apparatus to measure thermophysical properties of wind tunnel heat transfer models / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Richard F. Romanowski, Ira H. Steinberg, Langley Research Center, and Grumman Aerospace Corporation (page images at HathiTrust)
Lateral conduction effects on heat-transfer data obtained with the phase-change paint technique / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by George Maise, Michael J. Rossi, Langley Research Center, and Grumman Aerospace Corporation (page images at HathiTrust)
An electronic system for measuring thermophysical properties of wind tunnel models / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by Richard R. Corwin, Joseph S. Kramer, Langley Research Center, and Beta Industries (page images at HathiTrust)
Calibration of transonic and supersonic wind tunnels / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 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)
F-15 rotary balance data for an angle-of-attack range of 8⁰ to 90⁰ / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : for sale by the National Technical Information Service], 1982), by Billy Barnhart, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
Helicopter rotor trailing edge noise / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Robert H. Schlinker, Roy K. Amiet, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
A visual investigation of turbulence in stagnation flow about a circular cylinder / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Willy Z. Sadeh, Herbert J. Brauer, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Colorado State University (page images at HathiTrust)
Analysis of rotary balance data for the F-15 airplane including the effect of conformal fuel tanks / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Billy Barnhart, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Real-time computer data system for the 40- by 80-foot wind-tunnel facility at Ames Research Center / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Joseph M. Cambra, Geno P. Tolari, Informatics Inc, and Ames Research Center (page images at HathiTrust)
Flutter studies to determine nacelle aerodynamic effects on a fan-jet transport model for two mount systems and two wind tunnels [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Moses G. Farmer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Spectroscopic analysis of electron-beam-induced fluorescence in hypersonic helium flow / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Mervin E. Hillard, Richard W. Storey, Stewart L. Ocheltree, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Transition Reynolds numbers of separated flows at supersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Howard K. Larson, Stephen J. Keating, 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 / (Washington, D.C. : 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)
Wind-tunnel investigation of a 3/8-scale automobile model over a moving-belt ground plane / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Thomas R. Turner, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Investigation of the aerodynamic characteristics of a 0.067-scale model of the x-15 airplane (configuration 3) at mach numbers of 2.29, 2.98, and 4.65 / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Arthur E. Franklin, Robert M. Lust, and Langley Research Center (page images at HathiTrust)
Electrode configurations for a wind-tunnel heater incorporating the magnetically spun electric arc / (Washington : National Aeronautics and Space Administration, [1962]), by Donald R. Boldman, John C. Fakan, Charles E. Shepard, and Lewis Research Center (page images at HathiTrust)
Full-scale wind-tunnel tests of a small unpowered jet aircraft with a T-Tail / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 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)
Effect of air contamination in a helium tunnel / (Washington : 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 / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by William A. Newsom 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 / (Washington, D.C. : 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)
Wind-tunnel investigation of a large 35 ̊swept-wing jet transport model with an external-flow jet-augmented double-slotted flap / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by Kiyoshi Aoyagi, Leo P. Hall, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Static longitudinal aerodynamic characteristics of close-coupled wing-canard configurations at Mach numbers from 1.60 to 2.86. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1971]), by Samuel M. Dollyhigh, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Evolution, calibration, and operational characteristics of the two-dimensional test section of the Langley 0.3-meter transonic cryogenic tunnel / ([Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Aerodynamic force measurements with a strain-gage balance in a cryogenic wind tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by 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)
Application of two design methods for active flutter suppression and wind-tunnel test results / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Wind-tunnel experiments on divergence of forward-swept wings / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Rodney H. Ricketts, Robert V. Doggett, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F-15 airplane / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
A Numerical simulation of three-dimensional flow in an adaptive wall wind tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], [1984]), by J. P. Mendoza 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 / (Washington, D.C. : National Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Recent modifications and calibration of the Langley Low-Turbulence Pressure Tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Robert J. McGhee, Jean M. Foster, William D. Beasley, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Wind tunnel wall interference (January 1980-May 1988) : a selected, annotated bibliography / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by Marie H. Tuttle, Karen L. Cole, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
Experimental results for the Eppler 387 airfoil at low Reynolds numbers in the Langley low-turbulence pressure tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by Robert J. McGhee, Betty F. Millard, Betty S. Walker, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
Low-speed wind-tunnel test of a STOL supersonic-cruise fighter concept / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by Paul L. Coe, Donald R. Riley, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
Modifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment / (Washington, D.C. : 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)
Cryogenic wind tunnels : a selected, annotated bibliography / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by Marie H. Tuttle, Karen L. Cole, Robert A. Kilgore, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊/ (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 Emma Jean Landrum, C. Donald Babb, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
A device for rapid determination of thermophysical properties of phase-change wind-tunnel models / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 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 / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by John S. Tripp, Taumi S. Daniels, and Langley Research Center (page images at HathiTrust)
A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Pierce L. Lawing, Charles L. Ladson, Jerry B. Adcock, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Evaluation of wind-tunnel gust response technique correlations with analytical and flight test results / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by 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)
Wind tunnel measurements in the wakes of structures / (Washington : 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)
Two dimensional aerodynamic interference effects on oscillating airfoils with flaps in ventilated subsonic wind tunnels / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by 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)
Wind tunnel interference factors for high-lift wings in closed wind tunnels / (Washington, D.C. : National Aeronautics and Space Administration, [1973]), by Robert G. Joppa, Langley Research Center, and University of Washington (page images at HathiTrust)
Wind tunnel measurements of three-dimensional wakes of buildings / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Earl Logan, Shu Ho Lin, Arizona State University, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and George C. Marshall Space Flight Center (page images at HathiTrust)
A simplified fourwall interference assessment procedure for airfoil data obtained in the Langley 0.3-meter transonic cryogenic tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987), by A. V. Murthy and Langley Research Center (page images at HathiTrust)
Aerofoil testing in a self-streamlining flexible walled wind tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by Mark Charles Lewis and Langley Research Center (page images at HathiTrust)
Recent research on V/STOL test limits at the University of Washington Aeronautical Laboratory / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Shojiro Shindo, William H. Rae, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Space shuttle phase B wind tunnel test database : summary report / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by J. L. Glynn, D. E. Poucher, and Langley Research Center (page images at HathiTrust)
Adaptive wall technology for minimization of wall interferences in transonic wind tunnels / (Washington, D.C. : 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by A. V. Murthy and Langley Research Center (page images at HathiTrust)
Design study of test models of maneuvering aircraft configurations for the National Transonic Facility / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
Calibration of the Langley 16-foot transonic tunnel with test section air removal / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Blake W. Corson, William B. Igoe, Jack F. Runckel, and Langley Research Center (page images at HathiTrust)
Flight investigation of V/STOL height-control requirements for hovering and low-speed flight under visual conditions / (Washington, D.C. : National Aeronautics and Space Administration, [1967]), by James R. Kelly, Perry L. Deal, John F. Garren, and Langley Research Center (page images at HathiTrust)
Aerodynamic loads on deployed canard surfaces and rocket nose section of the Apollo launch escape vehicle / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 1969), by William C. Moseley, Branch S. Phillips, Manned Spacecraft Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
Full-scale investigation of the aerodynamic characteristics of a model employing a sailwing concept / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Marvin P. Fink, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Static aerodynamic characteristics, pressure distributions, and RAM-air inflation of attached inflatable decelerator models at Mach 3.0 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by William D. Deveikis, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Some anomalies observed in wind-tunnel tests of a blunt body at transonic and supersonic speeds / (Washington : National Aeronautics and Space Administration ; Springfield, Va. for sale by the National Technical Information Service, 1976), by Joseph D. Brooks, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Wind-tunnel investigation of a V/STOL transport model with four pod-mounted lift fans / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by William A. Newsom, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Wind-tunnel investigation of aerodynamic characteristics of a 1/2-scale model of an ejection seat with a rigid-wing recovery system / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Sanger M. Burk, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Model wind-tunnel and flight investigation of a parawing -- lifting-body landing system / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Rodger L. Naeseth, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Wind-tunnel studies of effects of construction methods, design details, and canopy slots on the aerodynamic characteristics of small-scale all-flexible parawings / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Paul G. Fournier, William C. Sleeman, 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 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 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 / (Washington, D.C. : 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)
Low-speed wind-tunnel investigation of all-flexible twin-keel tension-structure parawings / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Paul G. Fournier, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Wind-tunnel investigation of the low-speed high-lift aerodynamics of a one-fifth scale variable-sweep supersonic transport / (Washington, D.C. : 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)
Dynamic response of a Mach 2.5 axisymmetric inlet with engine or cold pipe and utilizing 60 percent supersonic internal area contraction / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Joseph F. Wasserbauer, Lewis 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 / (Washington : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1969), by Lysle P. Parlett, James P. Shivers, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Aerodynamic characteristics of an oblate spheroid and a sphere at Mach numbers from 1.70 to 10.49 / (Washington, D.C. : 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 / (Washington, D.C. : 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)
An experimental investigation of the velocity fluctuations behind oscillating vanes / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969]), by Donald A. Buell, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
Static and dynamic stability derivatives of a model of a jet transport equipped with external-flow jet-augmented flaps / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 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 / (Washington, D.C. : 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)
Aerodynamic parameters of the Navion airplane extracted from flight data / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1972), by William T. Suit, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Effect of trailing edge geometry and thickness on the performance of certain turbine stator blading. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1972]), by Herman W. Prust, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
A wind-tunnel evaluation of analytical techniques for predicting static stability and control characteristics of flexible aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1972), by Irving Abel, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Rapid estimation of wind-tunnel corrections with application to wind-tunnel and model design / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Harry H. Heyson, United States National Aeronautics and Space Administration, and Langley Research Center (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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), 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 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Marion O. McKinney and Langley Research Center (page images at HathiTrust)
Dynamic response of a family of axisymmetric hammerhead models to unsteady aerodynamic loading / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 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 / (Washington, D.C. : 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)
Low-speed static wind-tunnel investigation of a half-span fuselage and variable-sweep pressure wing model / (Washington, D.C. : 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)
Wind-tunnel investigation of an external-flow jet-flap transport configuration having full-span triple-slotted flaps / (Washington : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 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 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Jerry B. Adcock, Marilyn E. Ogburn, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Wind-tunnel investigation of a four-engine externally blowing jet-flap STOL airplane model. [electronic resource] / (Washington, 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)
Flow visualization by elastic light scattering in the boundary layer of a supersonic flow / (Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, 2000), by G. C. Herring, Mervin E. Hillard, and Langley Research Center (page images at HathiTrust)
Effects of angle of attack and bluntness on the hypersonic flow over a 15 ̊semiapex cone in helium / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 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)
Full-scale wind-tunnel investigation of the longitudinal aerodynamic characteristics of the M2-F1 lifting body flight vehicle / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966), by Kenneth W. Mort, Berl Gamse, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Large-scale wind-tunnel investigation of an M1-L lifting body with an inflatable and a rigid afterbody / (Washington, D.C. : 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)
AEDC test facilities handbook. (Tullahoma, Tenn., Arnold Engineering Development Center, Air Force, 1959), by Arnold Engineering Development Center (page images at HathiTrust)
An experimental investigation of high amplitude panel flutter / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, U.S. G.P.O.], 1971), by H. P. Kappus, N. H. Zimmerman, C. E. Lemley, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Wind-tunnel measurements on a lifting rotor at high thrust coefficients and high tip-speed ratios / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia], 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)
Some aspects of the behavior of perforated transonic wind tunnel walls. (Providence, 1954), by P. F. Maeder (page images at HathiTrust; US access only)
The effect of the converging flow field of a tandem-test-section on longitudinal stability measurements / (Washington, D.C. : National Aeronautics and Space Administration, 1968), by Shojiro Shindo and Robert G. Joppa (page images at HathiTrust; US access only)
One component, magnetic, support and balance system for wind tunnel models / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by K. R. Sivier, M. Henderson, University of Michigan, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
An analysis of performance estimation methods for aircraft / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by Clinton E. Brown and Chuan Fang Chen (page images at HathiTrust; US access only)
A wind tunnel investigation of panel response to boundary layer pressure fluctuations at mach 1.4 and mach 3.5 / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by David Alan Bies (page images at HathiTrust; US access only)
A method of calculating wind tunnel interference factors for tunnels of arbitrary cross-section / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by Robert G. Joppa (page images at HathiTrust; US access only)
Design of a Schlieren optical system / (Seattle, Wash. : University of Washington, Aeronautical Laboratory, [1949]), by James H. Brown (page images at HathiTrust; US access only)
A wind tunnel investigation of the Deer Isle-Sedgwick Bridge. (McLean, Va. : U.S. Department of Transportation, Federal Highway Administration, Research, Development, and Technology ; Springfield, Va. : National Technical Information Service [distributor, 1988]), by Harold R. Bosch and United States. Federal Highway Administration. Structures Division (page images at HathiTrust)
Pursuit of power : NASA's Propulsion Systems Laboratory, No. 1 & 2 /, by Robert S. Arrighi and United States. NASA History Division (page images at HathiTrust)
Large-scale tests of an airplane model with a double-Delta wing, including longitudinal and lateral characteristics and ground effects / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Victor R. Corsiglia, Joseph P. Morelli, David G. Koenig, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Real-helium hypersonic flow parameters for pressures to 3600 atmospheres and temperatures to 15 000° K / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 2215], 1968), by Charles G. Miller, Sue E. Wilder, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Experimental aerodynamics, (New York, Chicago, Pitman publishing corporation, [c1940]), by Henry Christensen Pavian and Phillip Lincoln Michel (page images at HathiTrust)
Smoke streams : visualized air flow / (New York : Coward-McCann, 1943), by Charles Townsend Ludington (page images at HathiTrust)
Supersonic wind tunnel tests of ring-wing configurations /, by Leon H. Schindel, United States. Air Force. Air Research and Development Command. sponsor, and Wright Air Development Center issuing body (page images at HathiTrust)
NO-O chemiluminescent reaction in a low-density wind tunnel /, 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)
The generation of gusts in a wind tunnel and measurement of unsteady lift on an airfoil /, by L. C. Garby, J. D. Schetzer, A. M. Kuethe, United States. Air Force. Air Research and Development Command. sponsor, University of Michigan, and Wright Air Development Center (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)
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)
Investigation of the I-40 Jet-Propulsion Engine in the Cleveland Altitude Wind Tunnel (Washington, D.C. : National Advisory Committee for Aeronautics, [1948]), by Richard L. Golladay, Stanley L. Gendler, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Flight Propulsion Research Laboratory (page images at HathiTrust)
Investigation of the I-40 Jet-Propulsion Engine in the Cleveland Altitude Wind Tunnel (Washington, D.C. : National Advisory Committee for Aeronautics, [1948]), by Reece V. Hensley, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Flight Propulsion Research Laboratory (page images at HathiTrust)
Preliminary investigation of a variable Mach number two-dimensional supersonic tunnel of fixed geometry / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by William J. Nelson, Frederick Bloetscher, 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)
Studies of the use of Freon-12 as a testing medium in the Langley low-turbulence pressure tunnel / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Albert E. Von Doenhoff, Albert L. Braslow, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
The development of an 8-inch by 8-inch slotted tunnel for Mach numbers up to 1.28 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1955), by B. H. Little, James M. Cubbage, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Wind tunnel simulation of head-on bow wave-blast wave interactions /, by David L. Merritt, P. M. Aronson, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
A cold flow field experimental study associated with a two-dimensional multiple nozzle /, by Jerry L. Wagner 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. /, 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. /, by R. L. P. Voisinet, H. U. Meier, Roland E. Lee, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
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)
Development and calibration of an aerodynamic disturbance test facility. Volume I: executive summary. Final report. (1978), by Richard H. Klein, Henry R. Jex, A. A. Blauvelt, and Irving Louis Ashkenas (page images at HathiTrust)
Development and calibration of an aerodynamic disturbance test facility. Volume II: development of requirements and preliminary design. Final report. (1978), by Richard H. Klein, Irving Louis Ashkenas, and Henry R. Jex (page images at HathiTrust)
Development and calibration of an aerodynamic disturbance test facility. Volume III: construction, calibration and operation. Final report. (1978), by Richard H. Klein, A. A. Blauvelt, and P. G. Van Valkenburgh (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)
Investigation of axially symmetric and two-dimensional multinozzles for producing supersonic streams / (Washington, D.C. : National Advisory Committee for Aeronautics, [1952]), by Eli Reshotko, Rudolph C. Haefeli, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
Altitude-wind-tunnel investigation of Westinghouse 19B-2 19B-8, and 19XB-1 jet-propulsion engines (Washington, D.C. : National Advisory Committee for Aeronautics, [1948]), by William A. Fleming, Robert O. Jr Dietz, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
Investigation of the I-40 Jet-Propulsion Engine in the Cleveland Altitude Wind Tunnel (Washington, D.C. : National Advisory Committee for Aeronautics, [1948]), by Richard P. Krebs, Frederick C. Foshag, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Flight Propulsion Research Laboratory (page images at HathiTrust)
Altitude-wind-tunnel investigation of Westinghouse 19B-2 19B-8, and 19XB-1 jet-propulsion engines (Washington, D.C. : National Advisory Committee for Aeronautics, [1948]), by Bemrose Boyd, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
Altitude-wind-tunnel investigation of Westinghouse 19B-2 19B-8, and 19XB-1 jet-propulsion engines (Washington, D.C. : National Advisory Committee for Aeronautics, [1948]), by Richard P. Krebs, Frank L. Suozzi, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
Altitude-wind-tunnel investigation of a 4000-pound-thrust axial-flow turbojet engine (Washington, D.C. : National Advisory Committee for Aeronautics, [1948]), by William A. Fleming, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Flight Propulsion Research Laboratory (page images at HathiTrust)
Investigation of the aerodynamic and icing characteristics of a recessed fuel cell vent assembly (Washington, D.C. : National Advisory Committee for Aeronautics, [1948]), by Robert S. Ruggeri, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Flight Propulsion Research Laboratory (page images at HathiTrust)
Altitude-wind-tunnel investigation of Westinghouse 19B-2 19B-8, and 19XB-1 jet-propulsion engines (Washington, D.C. : National Advisory Committee for Aeronautics, [1948]), by Robert O. Dietz, John K. Kuenzig, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
Altitude-wind-tunnel investigation of Westinghouse 19B-2 19B-8, and 19XB-1 jet-propulsion engines (Washington, D.C. : National Advisory Committee for Aeronautics, [1948]), by William A. Fleming, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Lewis Flight Propulsion Laboratory (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)
Preliminary investigation of shock-wave reflections in a small closed ballistic range with various types of walls / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Alexander Peter Sabol, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (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 / (Washington, D.C. : 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. NACA research memorandum (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)
Some possibilities of using gas mixtures other than air in aerodynamic research / (Washington, D.C. : 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 / (Washington, D.C. : 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 / ([Albuquerque, N.M.] : 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)
Electrical operations manual for the Sandia Corporation twelve-inch wind tunnel / ([Albuquerque, N.M.] : Sandia Corporation ; Washington, D.C. : Available from the Office of Technical Services, Department of Commerce, [1958]), by Mahlon George Baker and Sandia Corporation (page images at HathiTrust)
Wind tunnel supply headers /, by Anders S. Platou, U.S. Army Ballistic Research Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
Ballistic Research Laboratories' wind tunnel compressor plant /, by Ernest P. Reklis and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
Cooling water system, compressor plant no. 1 /, by Ernest P. Reklis and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
Upper atmosphere O-atom densities by wind tunnel simulation of nitric oxide releases /, by D. Golomb, R. Earl Good, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
The NOL 3 megawatt research arc /, 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 /, by A Leonas, F. Regan, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
Multiple pressure transducer banks and their application /, by D. B. Risher and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
A wind tunnel free-flight data-reduction program for either spinning or non spinning models utilizing data from a single plane /, by Charles E. Knadler 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 /, by Donald M Wilson and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
The sonic throat method and real gas one-dimensional flow : an application to air and nitrogen /, by Richard L. Humphrey, Jerry L. Wagner, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
The joint NOL/RAE/WRE research program on bomb dynamics., by Frank J Regan, J. F. Tanner, J. H. W. Shannon, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
NOL mach 18 hypervelocity research tunnel / (Ft. Belvoir Defense Technical Information Center, 29 AUG 1974), by Ray H. Cornett, Alton G Keel, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
Use of phase-change paints to study fin-body interference heating /, by Jr. Gillerlain and Naval Surface Weapons Center. : White Oak Laboratory (page images at HathiTrust)
Influence of roughness on heat transfer and transition : ART Program Data Report. /, by R. E. Phinney, F. P. Baltakis, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
Tables of interference factors for use in wind-tunnel and ground-effect calculations for VTOL-STOL aircraft. (Washington, National Aeronautics and Space Administration, 1962), by Harry H. Heyson (page images at HathiTrust; US access only)
Wind tunnel/flight data correlation (u)., by James A. Behal, Donald E. Simons, Milo H. Belgen, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor North American Rockwell Corporation. Columbus Division (page images at HathiTrust)
Wind tunnel/flight data correlation (u)., by James A. Behal, Donald E. Simons, Milo H. Belgen, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor North American Rockwell Corporation. Columbus Division (page images at HathiTrust)
Use of strained coordinate perturbation method in transonic aeroelestic computations /, by P. Guruswamy, sponsor Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Northrop Corporation. Aircraft Division (page images at HathiTrust)
Wind tunnel/flight data correlation (u)., by James A. Behal, Donald E. Simons, Milo H. Belgen, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor North American Rockwell Corporation. Columbus Division (page images at HathiTrust)
An experimental study of the distribution of convective heat transfer to a large-scale model of parachute cloth /, by E. R. G. Eckert, K. M. Krall, C. J. Scott, M. Ruiz-Urbieta, J. E. Anderson, sponsor Wright-Patterson Air Force Base (Ohio), sponsor University of Minnesota, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Pressure distribution during parachute opening., by H. D. Melzig, P. K. Schmidt, sponsor Deutsche Forschungsanstalt für Luft- und Raumfahrt (1961-1969), and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Investigation of ablation effects on hypersonic dynamic stability of a 10 cone /, by Dave R. Moore, Thomas C. Pope, Charles J. Stalmach, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor LTV Aerospace Corporation (page images at HathiTrust)
Aerodynamic Deployable Decelerator Performance-Evaluation Program : Phase 2 /, by E. Bloetscher, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Goodyear Aerospace Corporation (page images at HathiTrust)
Reports on wind tunnel experiments in aerodynamics (with five plates) (Washington, 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 / (Washington, D.C. : The Commission : Available from Gpo Sales Program, Division of Technical Information and Document Control, U.S. Nuclear Regulatory Commission ; Springfield, Va. : National Technical Information Service, 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)
Instrumentation of the ames supersonic free-flight wind tunnel / (Washington, DC : National Advisory Committee for Aeronautics, [1952]), by Robert O. Briggs, Stanley F. Schmidt, William J. Kerwin, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Ames Research Center (page images at HathiTrust)
Tests of submerged duct installation on a modified fighter airplane in the Ames 40- by 80-foot wind tunnel / (Washington, D.C. : National Advisory Committee for Aeronautics, [1947]), by Norman J. Martin, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Ames Research Center (page images at HathiTrust)
Boundary-layer measurements on several porous materials with suction applied / (Washington, D.C. : National Advisory Committee for Aeronautics, [1952]), by George B. McCullough, Bruno J. Gambucci, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Ames Research Center (page images at HathiTrust)
Evaluation of the T-755/GMQ-20 wind speed and direction transmitter /, by Russell M. Peirce and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Study of real gas and heat transfer effects on the design of hotshot wind tunnels / (Albuquerque, New Mexico : Sandia Corporation, Technical Information Division ; Washington, D.C. : Available from the Office of Technical Services, Dept. of Commerce, [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)
Wind tunnel/flight data correlation (u)., by James A. Behal, Donald E. Simons, Milo H. Belgen, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor North American Rockwell Corporation. Columbus Division (page images at HathiTrust)
Visualization of secondary-flow phenomena in blade row / (Washington, D.C. : National Advisory Committee for Aeronautics, [1952]), by H. Z. Herzig, G. R. Costello, A. G. Hansen, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
Multiple-source Schlieren system (transonic wind tunnel) / (Albuquerque, N.M. : Sandia Corporation, Technical Information Division ; Washington, D.C. : Available from the Office of Technical Services, Dept. of Commerce, 1960), by H. R. Spahr, R. E. Kyrlach, and Sandia Corporation (page images at HathiTrust)
Pressure and heat transfer measurements for hypersonic flows over expansion corners and ahead of ramps / (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1963-1964), by Louis G. Kaufman, sponsor Air Force Flight Dynamics Laboratory (U.S.), issuing agency United States. Air Force. Systems Command. Aeronautical Systems Division, and sponsor Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
Heat transfer measurements in cold wind tunnels /, by H. L. Moody, K. Jechel, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Air Force Wright Aeronautical Laboratories, and Calif.) PDA Engineering (Firm : Santa Ana (page images at HathiTrust)
Control effectiveness of transverse jets interacting with a high-speed free stream., by J. W. Barnes, H. H. Tang, J. G. Davis, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Douglas Aircraft Company. Santa Monica Division (page images at HathiTrust)
Advanced ejection seat for high dynamic pressure escape wind tunnel test report /, by J. O. Bull, R. F. Yurczyk, D. T. Ther, sponsor Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Boeing Military Airplane Company (page images at HathiTrust)
Longitudinal airplane dynamics wind tunnel test equipment /, by O. B. Tufts, A. H. Zimmerman, R. C. MacArthur, G. R. Duryea, issuing body Wright Air Development Center, sponsor United States. Air Force. Air Research and Development Command, and sponsor Cornell Aeronautical Laboratory (page images at HathiTrust)
Aerodynamic applications of plasma wind tunnels /, by Jackson R. Stalder, Boris Ragent, Charles E. Noble, Frederick K. Goodwin, United States. Air Force. Air Research and Development Command. issuing agency, and United States. Wright Air Development Center. sponsor (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)
Pressure distribution in the wake of two bodies revolution at transonic and supersonic speeds /, by Helmut G. Heinrich, R. Sheldon Hess, sponsor University of Minnesota. Department of Aerospace Engineering and Mechanics, sponsor Wright-Patterson Air Force Base (Ohio), and sponsor United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
High speed smoke flow visualization /, by Stephen M. Batill, T. J. Mueller, Robert C. Nelson, issuing agency Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor University of Notre Dame. Department of Aerospace and Mechanical Engineering (page images at HathiTrust)
Preliminary experiments on the simulation of gusts in a wind tunnel /, by Arnold M. Kuethe, R. L. Roensch, L. C. Garby, J. D. Schetzer, sponsor United States. Air Force. Air Research and Development Command, issuing body Wright Air Development Center, and sponsor University of Michigan. Department of Aeronautical Engineering (page images at HathiTrust)
Study of parachute scale effects /, by William B. Walcott, sponsor Technology Incorporated, and sponsor 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 /, by Rudolph Hermann, United States. Air Force. Air Research and Development Command. issuing agency, United States. Wright Air Development Center. sponsor, sponsor Aerospace Research Laboratories (U.S.), sponsor University of Minnesota, and sponsor Rosemount Aeronautical Laboratories (page images at HathiTrust)
A theoretical analysis of a new type of heater for an intermittent hypersonic wind tunnel /, by Antonio Ferri, Victor Zakkay, Paul A. Libby, sponsor United States. Air Force. Air Research and Development Command, and issuing body Wright Air Development Center (page images at HathiTrust)
Calibration of the AEDC-PWT 16-Foot transonic tunnel aerodynamic test section at various Reynolds numbers /, by F. M. Jackson, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
Influence of wind tunnel noise on the location of boundary-layer transition on a slender cone at Mach numbers from 0.2 to 5.5., by N. Sam Dougherty, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
Flow visualization techniques for use in hypersonic wind tunnels /, by R. W. Rhudy, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
Flow visualization photographs of a yawed tangent ogive cylinder at Mach number 2 /, by J. H. Jones, J. E. O'Hare, Arnold Engineering Development Center. sponsor, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
Model study of the exhaust flow noise of the proposed AEDC high Reynolds number tunnel /, by J. E. Robertson, sponsor Wyle Laboratories, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
Low-density hypervelocity wind tunnel diffuser performance /, by M. W. Milligan, J. F. Bailey, Knoxville. Department of Mechanical and Aerospace Engineering niversity of Tennessee, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
Calibration and performance of the AEDC/VKF Tunnel C, Mach Number 4, Aerothermal Wind Tunnel /, by W. T. Strike, sponsor Calspan Field Services, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
Perforated wall noise in the AEDC-PWT 16-ft and 4-ft transonic tunnels /, by O. P. Credle, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
Force and pressure tests of an AGARD Calibration Model B at a Mach number of 10 /, by R. K. Matthews, L. L Trimmer, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
Laser-Raman flow-field diagnostics of two large hypersonic test facilities /, by W. D. Williams, L. L. Price, H. M. Powell, D. A. Wagner, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
An analytic investigation of accuracy requirements for onboard instrumentation and film data for dynamically scaled wind tunnel drop models /, by K. S. Keen, R. L. Arterbury, C. H. Morgret, Inc. Sverdrup Technology, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
Comparisons of free-flight and wind tunnel data on slender cones /, by B. J. Griffith, Leo G. Siler, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
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)
Wind tunnel testing of interactions of high altitude rocket plumes with the free stream /, by H. K. Smithson, D. L. Whitfield, L. L. Price, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
Influence of wind tunnel noise on the location of boundary-layer transition on a slender cone at Mach numbers from 0.2 to 5.5., by N. Sam Dougherty, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
Visualization of the flow field about parachute canopy models and approximation of canopy pressure distributions /, by Charles A. Babish, Willard C. Hunter, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and United States. Air Force. Systems Command. Research and Technology Division. issuing body (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 /, by W. T. Strike, S. Pate, Inc. sponsor ARO, United States. Air Force. Air Research and Development Command. sponsor, and Arnold Engineering Development Center. issuing body (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 /, by Rudolf Hermann, Donald Olson, Frederick Moynihan, United States. Air Force. Office of Scientific Research. issuing body, Rosemount Aeronautical Laboratories. sponsor, and University of Minnesota. Institute of Technology. sponsor (page images at HathiTrust)
An analytical study of the dynamics of spinning aircraft., by John H. Wykes, Richard A. Collins, Gilbert R. Casteel, United States. Air Force. Air Research and Development Command. issuing body, Wright Air Development Center sponsor, and sponsor North American Aviation (page images at HathiTrust)
Boundary layer transition at supersonic speeds : three dimensional roughness effects (spheres) /, by E. R. Van Driest, C. B. Blumer, United States. Air Force. Office of Scientific Research. issuing body, and North American Aviation. Space and Information Systems Division. sponsor (page images at HathiTrust)
Stability derivatives of a 10° cone executing planar and nonplanar motion at Mach 14 /, by Kevin E. Yelmgren, Otto Walchner, Frank M. Sawyer, issuing body Aerospace Research Laboratories (U.S.), and sponsor Hypersonic Research Laboratory (U.S.) (page images at HathiTrust)
Tests of a wind tunnel flutter model., by Benjamin Smilg and issuing agency United States. Army Air Forces. Air Matériel Command (page images at HathiTrust)

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