Aerodynamics -- Testing

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• Aerodynamics
• Dynamics -- Testing
• Fluid dynamics -- Testing
• Airplanes -- Testing
• Testing

• Aerodynamic heating -- Testing
• Aerodynamic load -- Testing
• Aerodynamics, Hypersonic -- Testing
• Aerodynamics, Supersonic -- Testing
• Aerodynamics, Transonic -- Testing
• Aeroelasticity -- Testing
• Angle of attack (Aerodynamics) -- Testing
• Blades -- Testing
• Boundary layer -- Testing
• Drag (Aerodynamics) -- Testing
• Flutter (Aerodynamics) -- Testing
• Gas flow -- Testing
• Ground-cushion phenomenon -- Testing
• Leading edges (Aerodynamics) -- Testing
• Lift (Aerodynamics) -- Testing
• Mach number -- Testing
• Pitching (Aerodynamics) -- Testing
• Spin (Aerodynamics) -- Testing
• Stability of airplanes -- Testing
• Stability of helicopters -- Testing
• Stability of rockets -- Testing
• Vortex-motion -- Testing
• Aerodynamics -- Supersonic -- Testing
• Airplanes -- Parawings -- Aerodynamics -- Testing
• Automobiles -- Aerodynamics -- Testing
• Cone -- Aerodynamics -- Testing
• Cylinders -- Aerodynamics -- Testing
• Guided missiles -- Aerodynamics -- Testing
• Heat -- Transmission -- Aerodynamics -- Testing
• Launch vehicles (Astronautics) -- Aerodynamics -- Testing
• Lunar excursion module -- Aerodynamics -- Testing
• Parachutes -- Aerodynamics -- Testing
• Shells (Engineering) -- Aerodynamics -- Testing
• Space vehicles -- Aerodynamics -- Testing
• Transport planes -- Aerodynamics -- Testing

• Investigation of Axisymmetric and nonaxisymmetric nozzels installed on a 0.10-scale F-18 protype airplane model / Francis J. Capone and Bobby L. Berrier. (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 Francis J. Capone (page images at HathiTrust)
• Experimental investigation of tangential blowing applied to a subsonic V/STOL inlet / Richard R. Burley. (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 Richard R. Burley (page images at HathiTrust)
• A common geometric data-base approach for computer-aided manufacturing of wind-tunnel models and theoretical aerodynamic analysis / Michael J. See, James V. Cozzolongo. (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 Michael J. See (page images at HathiTrust)
• Full-scale investigation of the aerodynamic characteristics of a model employing a sailwing concept / Marvin P. Fink. (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 (page images at HathiTrust)
• Transition Reynolds numbers of separated flows at supersonic speeds / by Howard K. Larson and Stephen J. Keating, Jr. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]), by Howard K. Larson (page images at HathiTrust)
• Static longitudinal stability characteristics of various Mercury escape configurations and of a proposed alternate escape configuration for Mach numbers of 0.05 to 9.60 / by Robert P. Smith and William C. Moseley, Jr. (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Robert P. Smith (page images at HathiTrust)
• A compilation of wind-tunnel heat-transfer measurements on the afterbody of the Project Mercury capsule reentry configuration / by Kenneth C. Weston and Joanna E. Swanson. (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Kenneth C. Weston (page images at HathiTrust)
• Research on blunt-faced entry configurations at angles of attack Between 60° and 90° / by William H. Phillips (Washington D.C. : National Aeronautics and Space Administration, 1960), by William H. Phillips (page images at HathiTrust)
• Stability and control characteristics at a Mach number of 1.41 of a variable-sweep airplane configuration capable of low-level supersonic attack-outer wing swept 75°and 108° / by Ross B. Robinson and Paul W. Howard. (Washington D.C. : National Aeronautics and Space Administration, 1960), by Ross B. Robinson (page images at HathiTrust)
• Performance of a composite solid propellant at simulated high altitudes / by Carl C. Ciepluch. (Washington D.C. : National Aeronautics and Space Administration, 1959), by Carl C. Ciepluch (page images at HathiTrust)
• Subsonic aerodynamic characteristics of an airplane configuration utilizing a variable-sweep wing having a free-floating apex / Edward C. Polhamus and Alexander D. Hammond. (Washington, D.C. : National Aeronautics and Space Administration : Scientific and Technical Information Branch, 1965), by Edward C. Polhamus (page images at HathiTrust)
• Experimental investigation of base heating and rocket hinge moments for a simulated missile through a Mach number range of 0.8 to 2.0 / by Bruce G. Chiccine, Alfred S. Valerino, and Arthur M. Shinn. (Washington D.C. : National Aeronautics and Space Administration, 1959), by Bruce G. Chiccine (page images at HathiTrust)

• Performance of laser glazed ZrO2 TBCs in cyclic oxidation and corrosion burner test rigs / I. Zaplatynsky. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by I. Zaplatynsky (page images at HathiTrust)
• Aerodynamic heating tests of missile stabilizers in a free jet at Mach number 2 / by Louis F. Vosteen. (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Louis F. Vosteen (page images at HathiTrust)
• Investigation of the loading characteristics of the lifting surfaces and the speed brakes of a 0.067-scale model of the north american x-15 airplane (configuration 3) at Mach numbers of 2.29, 2.98, and 4.65 / by H. Norman Silvers, Julia A. Lancaster, and Jane S. Wills. (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Norman H. Silvers (page images at HathiTrust)

• Effects of spanwise blowing on the surface pressure distributions and vortex-lift characteristics of a trapezoidal wing-strake configuration / James F. Campbell and Gary E. Erickson. ([Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1979), by James F. Campbell (page images at HathiTrust)
• Aerodynamic loads on deployed canard surfaces and rocket nose section of the Apollo launch escape vehicle / William C. Moseley, Jr., and Branch S. Phillips. (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 (page images at HathiTrust)
• Force measurements on axisymmetric models with hammerhead noses at transonic speeds / by Bruno J. Gambucci and Robert D. Robinson. (Washington, D.C. : National Aeronautics and Space Administration, 1967), by Bruno J. Gambucci (page images at HathiTrust)
• Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing / by Earl R. Keener. (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Earl R. Keener (page images at HathiTrust)
• Heat transfer and pressure distribution at a mach number of 6.8 on bodies with conical flares and extensive flow separation.&bJonh V. Becker and Peter F. Korycinski. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by John V. Becker (page images at HathiTrust)
• An experimental pressure-distribution investigation of interference effects produced at a Mach number of 3.11 by wedge- shaped bodies located under a triangular wing / by Lowell E. Hasel. (Washington D.C. : National Aeronautics and Space Administration, 1959), by Lowell E. Hasel (page images at HathiTrust)

• Experimental determination of flow-interference effects of wing-mounted two-dimensional, full-capture propulsion nacelles in close proximity to a vehicle body at a Mach number of 6 / Walter A. Vahl. (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 Walter A. Vahl (page images at HathiTrust)
• Hypersonic flutter analysis using measured static aerodynamic derivatives, and comparison with experiment / Robert C. Goetz. (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1969), by Robert C. Goetz (page images at HathiTrust)

• Static stability and control characteristics of two large-dihedral right triangular pyramid lifting reentry configurations at a mach number of 3.05 / by Charles F. Whitcomb and Willard E. Foss, Jr. (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Charles F. Whitcomb (page images at HathiTrust)
• Hypersonic viscous drag on cones in rarefied flow / Marvin I. Kussoy. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by M. I. Kussoy (page images at HathiTrust)
• Transonic and supersonic ejection release characteristics of six dynamically scaled external-store shapes from an 0.086-scale model of a current fighter airplane / by William F. Hinson. (Washington D.C. : National Aeronautics and Space Administration, 1959), by William F. Hinson (page images at HathiTrust)
• Stability and control characteristics at low subsonic speeds of an airplane configuration having two types of variable-sweep wings / by Bernard Spencer, Jr. (Washington D.C. : National Aeronautics and Space Administration, 1960), by Bernard Spencer (page images at HathiTrust)
• An experimental pressure-distribution investigation of interference effects produced at a Mach number of 3.11 by wedge- shaped bodies located under a triangular wing / by Lowell E. Hasel. (Washington D.C. : National Aeronautics and Space Administration, 1959), by Lowell E. Hasel (page images at HathiTrust)
• Heat-transfer measurements on a blunt spherical-segment nose to a Mach number of 15.1 and flight performance of the rocket-propelled model to a Mach number of 17.8 / by Charles B. Rumsey and Dorothy B. Lee. (Washington D.C. : National Aeronautics and Space Administration, 1959), by Charles B. Rumsey (page images at HathiTrust)

• Effects of vertical-tail size and a ventral fin on the static lateral and directional stability derivatives of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speeds / by Walter B. Olstad. (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Walter B. Olstad (page images at HathiTrust)
• Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing / by Earl R. Keener. (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Earl R. Keener (page images at HathiTrust)
• Transonic pressure distributions over protuberances and adjacent areas in proximity to the nose of a launch vehicle / by James A. Blackwell, Jr. (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1966), by James A. Blackwell (page images at HathiTrust)
• An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics / by Robert V. Doggett, Jr., A. Gerald Rainey, and Homer G. Morgan. (Washington D.C. : National Aeronautics and Space Administration, 1959), by Robert V. Doggett (page images at HathiTrust)
• Transonic and supersonic ejection release characteristics of six dynamically scaled external-store shapes from an 0.086-scale model of a current fighter airplane / by William F. Hinson. (Washington D.C. : National Aeronautics and Space Administration, 1959), by William F. Hinson (page images at HathiTrust)
• The transonic aerodynamic characteristics of two variable-sweep airplane configurations capable of low-level supersonic attack / by Ralph P. Bielat, A. Warner Robins, and William J. Alford, Jr. (Washington D.C. : National Aeronautics and Space Administration, 1960), by Ralph P. Bielat (page images at HathiTrust)

• A simulation study of the flight dynamics of elastic aircraft / Martin R. Waszak, John B. Davidson, and David K. Schmidt. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987), by Martin R. Waszak (page images at HathiTrust)

• Aerodynamic characteristics of several cranked leading-edge wing-body combinations at Mach numbers from 0.4 to 2.94 / by Edward J. Hopkins, Raymond M. Hicks, and Ralph L. Carmichael (Ames Research Center). (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Edward J. Hopkins (page images at HathiTrust)
• Static longitudinal stability characteristics of various Mercury escape configurations and of a proposed alternate escape configuration for Mach numbers of 0.05 to 9.60 / by Robert P. Smith and William C. Moseley, Jr. (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Robert P. Smith (page images at HathiTrust)
• Low-speed measurements of oscillatory lateral stability derivatives of a model of 60° delta-wing bomber / by John W. Paulson. (Washington, D.C. : National Aeronautics and Space Administration, 1959), by John W. Paulson (page images at HathiTrust)
• Some measurements of the dynamic and static stability of two blunt-nosed, low-fineness-ratio bodies of revolution in free flight at M=4 / by Barbara J. Short and Simon C. Sommer. (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Barbara J. Sort (page images at HathiTrust)

• Development and testing of a pneumatic scraper blade for conveyor belt cleaning / by C.A. Rhoades, S.G. Grannes, and T.L. Hebble. (Washington, D.C. : U.S. Dept. of the Interior, Bureau of Mines, 1989), by C. A. Rhoades (page images at HathiTrust)
• Surface pressure measurements at two tips of a model helicopter rotor in hover / R.B. Gray ... [et al.] ; prepared for Langley Research Center under Contract NAS1-15158. (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 R. B. Gray (page images at HathiTrust)

• Investigations of a flow field surrounding circular-arc boattail nozzles at subsonic speeds / William K. Abeyounis and Lawrence E. Putnam. (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 William Kelly Abeyounis (page images at HathiTrust)
• Wind-tunnel investigation of a 3/8-scale automobile model over a moving-belt ground plane / Thomas R. Turner. (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 (page images at HathiTrust)

• Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration / Richard J. Re and David E. Reubush. (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], 1979), by Richard J. Re (page images at HathiTrust)
• An analysis of flight test data on the C-141A aircraft / by J. H. Paterson ... [et al.]. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1970) (page images at HathiTrust)
• An experimental investigation of dynamic ground effect / Pai Hung Lee, C. Edward Lan, and Vincent U. Muirhead. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987), by Pai Hung Lee (page images at HathiTrust)
• Deployment and performance characteristics of 5-foot-diameter (1.5 m) attached inflatable decelerators from Mach number 2.2 to 4.4 / by Herman L. Bohon and R. Miserentino. (Washington, DC : National Aeronautics and Space Administration, 1970), by Herman L. Bohon (page images at HathiTrust)
• Some measurements of the dynamic and static stability of two blunt-nosed, low-fineness-ratio bodies of revolution in free flight at M=4 / by Barbara J. Short and Simon C. Sommer. (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Barbara J. Sort (page images at HathiTrust)

• Analysis of preflutter and postflutter charactristics with motion-matched aerodynamic forces / Herbert J. Cunningham, Langley Research Center. ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Herbert J. Cunningham (page images at HathiTrust)
• Further experimental results on the influence of the turbulent boundary layer on panel flutter / Peter A. Gaspers, Jr., Lado Muhlstein, Jr., and Daniel N. Petroff. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Peter A. Gaspers (page images at HathiTrust)
• An experimental study of the influence of the turbulent boundary layer on panel flutter / Lado Muhlstein, Jr., Peter A. Gaspers, Jr., Dennis W. Riddle. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by Lado Muhlstein (page images at HathiTrust)
• Experimental investigation of the transonic flutter of simple thin truncated-cone panels / by Jean Gilman, Jr. (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Jean Gilman (page images at HathiTrust)
• Effects of boundary-layer suction and spoilers on transonic flutter derivatives for a midspan control surface on an upswept wing / John A. Wyss ... [et al.] (Washington, [D.C.] : National Aeronautics and Space Administration, 1960) (page images at HathiTrust)
• Experimental and calculated supersonic flutter characteristics of models of the x-15 horizontal and vertical tails / by William T. Lauten, Jr., and Robert W. Hess. (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by William T. Lauten (page images at HathiTrust)
• An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics / by Robert V. Doggett, Jr., A. Gerald Rainey, and Homer G. Morgan. (Washington D.C. : National Aeronautics and Space Administration, 1959), by Robert V. Doggett (page images at HathiTrust)

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