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Transonic wind tunnels

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• Aerodynamics, Transonic
• Wind tunnels

• Transonic aerodynamic characteristics of a variable-sweep airplane configuration having a 12-percent-thick wing and an inboard pivot location / (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Ralph P. Bielat, P. Kenneth Pierpont, and Langley Research Center (page images at HathiTrust)
• Longitudinal aerodynamic characteristics at transonic speeds of a V/STOL airplane configuration with a fixed delta wing having auxiliary variable-sweep outboard panels / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Arvo A. Luoma and Langley Research Center (page images at HathiTrust)
• Transonic flutter investigation of models of the X-15 airplane horizontal tail / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Lou S. Young, Samuel R. Bland, and Langley Research Center (page images at HathiTrust)
• High Reynolds number tests of a NASA SC(3)-0712(B) airfoil 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, 1985), by William G. Johnson, Otto Eichmann, Acquilla S. Hill, and Langley Research Center (page images at HathiTrust)
• Aerodynamic characteristics of a 0.0667-scale model of the X-15A-2 research airplane at transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1966), by James C. Patterson and Langley Research Center (page images at HathiTrust)
• Analysis of validation tests of the Langley pilot transonic cryogenic tunnel / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Edward J. Ray and Langley Research Center (page images at HathiTrust)
• Pressure distributions from high Reynolds number tests of a NASA SC(3)-0712(B) airfoil 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, 1985), by William G. Johnson, Otto Eichmann, Acquilla S. Hill, and Langley Research Center (page images at HathiTrust)
• Wall-interference assessment and corrections for transonic NACA 0012 airfoil data from various 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 Lawrence L. Green, Perry A. Newman, and Langley Research Center (page images at HathiTrust)
• Calibration of the 13- by 13-inch adaptive wall test section for the Langley O.3-meter transonic cryogenic 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 Raymond E. Mineck, Acquilla S. Hill, and Langley Research Center (page images at HathiTrust)
• Data quality analysis at the National Transonic Facility / (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 Pamela N. Stewart, Langley Research Center, and Wyle Laboratories (page images at HathiTrust)
• Realtime multi-plot graphics 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, 1990), by Michael S. Shipkowski, Langley Research Center, and Wyle Laboratories (page images at HathiTrust)
• Optimization of wave cancellation in variable porosity transonic wind tunnel flows / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by John William Davis and George C. Marshall Space Flight Center (page images at HathiTrust)
• A study of residual interference effects in adaptive wall testing of a 7-inch chord CAST-10-2/DOA 2 airfoil model / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by A. V. Murthy, Inc ViGYAN, and Langley Research Center (page images at HathiTrust)
• Aerodynamic loading characteristics at Mach numbers from 0.80 to 1.20 of a 1/10-scale three-stage scout model / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Thomas C. Kelly, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Description and calibration of the Langley 6- by 19-inch transonic tunnel / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Charles L. Ladson and Langley Research Center (page images at HathiTrust)
• Transonic wind-tunnel tests of an error-compensated static-pressure probe / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Francis J. Capone, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Transonic aerodynamic loading characteristics of a wing-body-tail combination having 52.5° sweptback wing of aspect ratio 3 with conical wing camber and body indentation for a design Mach number [square root of] 2 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Marlowe D. Cassetti, William B. Igoe, Richard J. Re, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Simulation of flight test conditions in the Langley pilot transonic cryogenic tunnel / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Robert A. Kilgore, Edward J. Ray, Jerry B. Adcock, and Langley Research Center (page images at HathiTrust)
• Description and calibration of the Langley 6- by 28-inch transonic tunnel / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Charles L. Ladson and Langley Research Center (page images at HathiTrust)
• Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by William J. Alford, William P. Handerson, Arvo A. Luoma, and Langley Research Center (page images at HathiTrust)
• To promote the national defense by authorizing a unitary plan for the construction of transsonic and supersonic wind-tunnel facilities and the establishment of an air engineering development center (H.R. 3434). ([Washington, D.C.] : [U.S. G.P.O.], [1949]), by United States House Committee on Armed Services, Carl Vinson, Jerome C. Hunsaker, and James Forrestal (page images at HathiTrust)
• Full committee hearing on H.R. 9612 and S. 3889 / ([Washington, D.C.] : [U.S. G.P.O.], [1950]), by United States House Committee on Armed Services (page images at HathiTrust)
• Subcommittee hearings on H.R. 3434, to promote the national defense by authorizing a unitary plan for the construction of transonic and supersonic wind-tunnel facilities and the establishment of an air engineering development center / ([Washington, D.C.] : [U.S. G.P.O.], [1949]), by United States. Congress. House. Committee on Armed Services. Subcommittee No. 3 (page images at HathiTrust)
• Full committee hearings on H.R. 2895, S. 509, S. 1267, S. 2382, S. 2380, S. 1560, H.R. 5876 / ([Washington, D.C.] : [U.S. G.P.O.], [1949]), by United States House Committee on Armed Services (page images at HathiTrust)
• High Reynolds number research : a workshop / (Washington : Scientific and Technical Information Office, National Aeronautics and Space Administration ; Springfield, Va. : for sale by National Technical Information Service, 1977), by Va.)) Workshop on High Reynolds Number Research ((1st : : 1976 : : Hampton, Donald D. Baals, and Joint Institute for Advancement of Flight Sciences (page images at HathiTrust)
• Effect of plug base contour on performance of a fully truncated plug nozzle with translating shroud / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Charles E. Mercer, Bobby L. Berrier, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Surface pressure distributions on 0.0628-scale models of proposed project fire space vehicles at Mach numbers from 0.25 to 4.63 / (Washington, D.C. : National Aeronautics and Space Administration, 1963), by Albin O. Pearson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Guide for users of 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], 1981), by Dennis E. Fuller, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Transonic wind-tunnel investigation of the effect of control span and large wing-tip nacelles on effectiveness of spoiler-slot-deflector controls on an unswept-wing fighter-type airplane / (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Dewey E. Wornom and Langley Research Center (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)
• 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)
• R4 airfoil data corrected for sidewall boundary-layer effects 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 Renaldo V. Jenkins and Langley Research Center (page images at HathiTrust)
• The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers / (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 Elizabeth B. Plentovich and Langley Research Center (page images at HathiTrust)
• Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed 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 Elizabeth B. Plentovich, Blair B. Gloss, and Langley Research Center (page images at HathiTrust)
• An experimental investigation of boundary layer and crossflow characteristics of the AMes 2- by 2-foot and 11- by 11-foot transonic wind-tunnel walls / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Gerald Edwin Matyk, Yasunori Kobayashu, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Performance test of laser velocimeter system for the Langley 16-Foot Transonic 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 James F. Meyers, United States. Army Aviation Systems Command. Aerostructures Directorate, and Langley Research Center (page images at HathiTrust)
• Plenum response to simulated disturbances of the model and fan inlet guide vanes in a transonic tunne / (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 Blair B. Gloss and Langley Research Center (page images at HathiTrust)
• Image degradation in 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], 1982), by W. L. Snow, William K. Goad, Alpheus W. Burner, 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 Reynolds number and Mach number on flow angularity probe sensitivity / (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 Leigh Ann Smith, Jerry B. Adcock, and Langley Research Center (page images at HathiTrust)
• A description of the active and passive sidewall-boundary-layer removal systems of the 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, Edward J. Ray, A. V. Murthy, and Langley Research Center (page images at HathiTrust)
• Static internal performance of single-expansion-ramp nozzles with various combinations of internal geometric parameters / (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 J. Re, Laurence D. Leavitt, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil 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, 1985), by William G. Johnson, Acquilla S. Hill, and Langley Research Center (page images at HathiTrust)
• Sensitivity analysis of cool-down strategies for a 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], 1982), by Jerry J. Thibodeaux and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Operating characteristics of the multiple critical venturi system and secondary calibration nozzles used for weight-flow measurements in the Langley 16-foot transonic 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 Bobby L. Berrier, Linda S. Bangert, Laurence D. Leavitt, and Langley Research Center (page images at HathiTrust)
• Simulaion of ideal-gas flow by nitrogen and other selected gases at cyogenic temperatures / (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 M. Hall, Jerry B. Adcock, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Comparison of experimental and theoretical turbulance reduction characteristics for screens, honeycomb, and honeycomb-screen combinations / (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, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• An application of multivariable design techniques to the control of 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], 1981), by Ernest S. Armstrong, John S. Tripp, 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)
• Force measurements on axisymmetric models with hammerhead noses at transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by Bruno J. Gambucci, Robert C. Robinson, and Ames Research Center (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 / (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Walter B. Olstad and Langley Research Center (page images at HathiTrust)
• Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Earl R. Keener and Flight Research Center (U.S.) (page images at HathiTrust)
• Principal results from wind-tunnel stability tests of several proposed space capsule models up to an angle of attack of 33° / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Howard S. Carter, Roland D. English, Ronald Kolenkiewicz, and Langley Research Center (page images at HathiTrust)
• A rigidly forced oscillation system for meaasuring dynamic-stability parameters in transonic and supersonic wind tunnels / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Albert L. Braslow, Cullen Q. Lee, Harleth G. Wiley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Evaluation of turbulence reduction devices for the Langley 8-foot Transonic Pressure Tunnel / (Washington, D.C. : National Aeronautics and Space Administration, 1981), by Marion O. McKinney, James Scheiman, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics / (Washington D.C. : National Aeronautics and Space Administration, 1959), by Robert V. Doggett, Homer G. Morgan, A. Gerald Rainey, and Langley Research Center (page images at HathiTrust)
• Effects of three spanwise twist variations on the longitudinal aerodynamic characteristics of a thin 45° sweptback highly tapered wing at transonic speeds / (Washington D.C. : National Aeronautics and Space Administration, 1959), by John P. Mugler and Langley Research Center (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 / (Washington D.C. : National Aeronautics and Space Administration, 1959), by Charles B. Rumsey, Dorothy B. Lee, and Langley Research Center (page images at HathiTrust)
• Numerical calculation of transonic flow about slender bodies of revolution / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971), by Frank R. Bailey, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Raymond E. Mineck and Langley Research Center (page images at HathiTrust)
• Mass flux similarity for slotted transonic-wind-tunnel walls / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by Joel L. Everhart, Suresh H. Goradia, and Langley Research Center (page images at HathiTrust)
• Evaluation of flow quality in two large NASA wind tunnels at transonic speeds / (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 Bill Harvey, F. Kevin Owen, P. Calvin Stainback, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Hardware and operating features of the adaptive wall test section for the Langley 0.3-meter transonic cryogenic 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, 1989), by Raymond E. Mineck (page images at HathiTrust)
• Wind tunnel blockage and support interference effects on winged-body models at Mach numbers from 0.6 to 1.0 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Bernard J. Blaha and Lewis Research Center (page images at HathiTrust)
• Effect of several geometric parameters on the static internal performance of three nonaxisymmetric nozzle concepts / (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 Bobby L. Berrier, Richard J. Re, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Some remarks on the design of transonic tunnels with low levels of flow unsteadiness / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1976), by Dennis G. Mabey, Langley Research Center, and Royal Aircraft Establishment (Great Britain). Structures Dept (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)
• 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)
• Sting-support interference on longitudinal aerodynamic characteristics of cargo-type airplane models at Mach 0.70 to 0.84 / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Donald L. Loving, Arvo A. Luoma, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Design features and operational characteristics of the Langley 0.3-meter transonic cryogenic tunnel / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Robert A. Kilgore and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Evaluation of a technique for determining airplane aileron effectiveness and roll rate by using an aeroelastically scaled model / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Irving Abel, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A theoretical and experimental study of unsteady flow processes in a Ludwieg tube wind tunnel / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by John D. Warmbrod, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low subsonic pressure distributions on three rigid wings simulating paragliders with varied canopy curvature and leading-edge sweep / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Paul G. Fournier, B. Ann Bell, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Experimental investigation at transonic speeds of pressure distributions over wedge and circular-arc airfoil sections and evaluation of perforated-wall interference / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Earl D. Knechtel and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transonic aerodynamic characteristics of a model of a supersonic fighter-bomber airplane with external fuel tanks and other modifications / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966), by James C. Ferris and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• 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)
• 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)
• 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)
• Transonic wind-tunnel investigation of the interference between a 45©� sweptback wing and a systematic series of four bodies / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Donald L. Loving, Dewey E. Wornom, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Transonic wind-tunnel investigation of an unswept wing in combination with a systematic series of four bodies / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by Bruce B. Estabrooks, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Steady-state characteristics of a differential-pressure system for evaluating angles of attack and sideslip of the Ranger IV vehicle / (Washington, D.C. : National Aeronautics and Space Administration, 1963), by E. Carson Yates, Annie G. Fox, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• A study of acoustic disturbances and means of suppression in ventilated transonic wind tunnel walls /, by N. Sam Dougherty, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• Calibration of the AEDC-PWT 16-ft transonic tunnel with the propulsion 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)
• 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)
• Aerodynamic characteristics of perforated walls for transonic wind tunnels /, by J. L. Jacocks, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• Tests of the ONERA calibration models in three transonic wind tunnels /, by Travis W. Binion, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, sponsor France. Office national d'études et de recherches aérospatiales, and Inc. ARO (page images at HathiTrust)
• The effect of plenum volume on the test section flow characteristics of a perforated wall transonic tunnel /, by C. F. Anderson, O. P. Credle, A. Anderson, Arnold Engineering Development Center. sponsor, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Measurement of the pressure fluctuations in the test section of the 1-foot transonic tunnel in the frequency range from 5 to 1250 cps /, by J. E. Robertson, Inc. ARO, 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)
• Documentation of the Phase III 0.192-scale Northrop/McDonnell-Douglas F-18 inlet performance test at mach numbers 0 to 1.55 /, by Jimmy Walker, Sverdrup Corporation. sponsor, United States. Naval Air Systems Command. sponsor, and United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• Fundamental studies of subsonic and transonic flow separation., by J. M. Wu, K. Anjaneyulu, Herbert Venghaus, L. Shen, R. Nygaard, C. H. Chen, K. C. Reddy, G. M. Elfstrom, Trevor H. Moulden, University of Tennessee (System). Space Institute. sponsor, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Experiments to assess the influence of changes in the tunnel wall boundary layer on transonic wall crossflow characteristics /, by R. F. Starr, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Noise generation in transonic wind tunnels /, by M. O. Varner, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Calculation of the boundary-layer growth in a Ludwieg tube /, by James C. Sivells, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Fundamental studies of subsonic and transonic flow separation., by J. M. Wu, United States. Air Force. Systems Command. Arnold Engineering Development Center. sponsor, and University of Tennessee (System). Space Institute. issuing body (page images at HathiTrust)
• An Investigation of three-dimensional wall interference in a variable porosity transonice wind tunnel /, by Travis W. Binion, United States. Air Force. Arnold Air Force Base. sponsor, United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body, and Inc. ARO (page images at HathiTrust)
• Application of linearized transonic theory to tunnel blockage interference /, by C. F. Lo, United States. Air Force. Arnold Air Force Base. sponsor, United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body, and Inc. ARO (page images at HathiTrust)

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