Transonic wind tunnels -- Equipment and suppliesSee also what's at your library, or elsewhere.
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Filed under: Transonic wind tunnels -- Equipment and supplies
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Filed under: Transonic wind tunnels- Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques (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)
- Wall-interference assessment and corrections for transonic NACA 0012 airfoil data from various wind tunnels (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 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 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Raymond E. Mineck, Acquilla S. Hill, and Langley Research Center (page images at HathiTrust)
- Computer program to improve Space Tracking and Data Acquisition Network station scheduling (National Aeronautics and Space Administration ;, 1966), by Walter D. Davis and Goddard Space Flight Center (page images at HathiTrust)
- Aerodynamic characteristics of a 0.0667-scale model of the X-15A-2 research airplane at transonic speeds (National Aeronautics and Space Administration ;, 1966), by James C. Patterson and Langley Research Center (page images at HathiTrust)
- Mass flux similarity for slotted transonic-wind-tunnel walls (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), by Joel L. Everhart, Suresh H. Goradia, and Langley Research Center (page images at HathiTrust)
- Transonic aerodynamic characteristics of a tailless fixed-wing supersonic transport model (National Aeronautics and Space Administration ;, 1966), by Edward J. Ray, Robert T. Taylor, and Langley Research Center (page images at HathiTrust)
- R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by James F. Meyers, United States. Army Aviation Systems Command. Aerostructures Directorate, and Langley Research Center (page images at HathiTrust)
- Guide for users of the National Transonic Facility (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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)
- Image degradation in Langley 0.3-meter transonic cryogenic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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)
- Hardware and operating features of the adaptive wall test section for the Langley 0.3-meter transonic cryogenic tunnel (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 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 (National Aeronautics and Space Administration ;, 1974), by Bernard J. Blaha and Lewis Research Center (page images at HathiTrust)
- Improvement in the quality of flow visualization in the Langley 0.3-meter transonic cryogenic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Jerry J. Thibodeaux 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 NASA SC(3)-0712(B) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by William G. Johnson, Otto Eichmann, Acquilla S. Hill, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by William G. Johnson, Otto Eichmann, Acquilla S. Hill, and Langley Research Center (page images at HathiTrust)
- Comparison of experimental and theoretical turbulance reduction characteristics for screens, honeycomb, and honeycomb-screen combinations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by James Scheiman, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Development of a distributed-parameter mathematical model for simulation of cryogenic wind tunnels (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by John S. Tripp and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- A study of residual interference effects in adaptive wall testing of a 7-inch chord CAST-10-2/DOA 2 airfoil model (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), by A. V. Murthy, Inc ViGYAN, and Langley Research Center (page images at HathiTrust)
- Adaptive wall technology for minimization of wall interferences in transonic wind tunnels (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by Stephen W. D. Wolf and Langley Research Center (page images at HathiTrust)
- Transonic wind-tunnel tests of an error-compensated static-pressure probe (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 (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)
- Aerodynamic loading characteristics at Mach numbers from 0.80 to 1.20 of a 1/10-scale three-stage scout model (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 28-inch transonic tunnel (National Aeronautics and Space Administration ;, 1975), by Charles L. Ladson and Langley Research Center (page images at HathiTrust)
- Simulation of flight test conditions in the Langley pilot transonic cryogenic tunnel (National Aeronautics and Space Administration ;, 1974), by Robert A. Kilgore, Edward J. Ray, Jerry B. Adcock, and Langley Research Center (page images at HathiTrust)
- Design features and operational characteristics of the Langley 0.3-meter transonic cryogenic tunnel (National Aeronautics and Space Administration ;, 1976), by Robert A. Kilgore and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-5655 (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)
- NASA TN D-5538 (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)
- Optimization of wave cancellation in variable porosity transonic wind tunnel flows (National Aeronautics and Space Administration ;, 1973), by John William Davis and George C. Marshall Space Flight Center (page images at HathiTrust)
- Force measurements on axisymmetric models with hammerhead noses at transonic speeds (National Aeronautics and Space Administration, 1967), by Bruno J. Gambucci, Robert C. Robinson, and Ames Research Center (page images at HathiTrust)
- A rigidly forced oscillation system for meaasuring dynamic-stability parameters in transonic and supersonic wind tunnels (National Aeronautics and Space Administration :, 1962), by Albert L. Braslow, Cullen Q. Lee, Harleth G. Wiley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-5469 (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)
- NASA TN D-3701 (National Aeronautics and Space Administration :, 1966), by James C. Ferris and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- Low subsonic pressure distributions on three rigid wings simulating paragliders with varied canopy curvature and leading-edge sweep (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 (National Aeronautics and Space Administration, 1959), by Earl D. Knechtel and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-1961 (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)
- NASA TN D-1966 (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)
- Description and calibration of the Langley 6- by 19-inch transonic tunnel (National Aeronautics and Space Administration ;, 1973), by Charles L. Ladson and Langley Research Center (page images at HathiTrust)
- NASA TN D-6582 (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)
- Transonic aerodynamic characteristics of a variable-sweep airplane configuration having a 12-percent-thick wing and an inboard pivot location (National Aeronautics and Space Administration, 1960), by Ralph P. Bielat, P. Kenneth Pierpont, and Langley Research Center (page images at HathiTrust)
- Transonic flutter investigation of models of the X-15 airplane horizontal tail (National Aeronautics and Space Administration, 1961), by Lou S. Young, Samuel R. Bland, and Langley Research Center (page images at HathiTrust)
- Air-flow and power characteristics of the Langley 16-foot transonic tunnel with slotted test section (National Advisory Committee for Aeronautics, 1952), by Vernon G. Ward, Merwin D. Pearson, Charles F. Whitcomb, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
- An experimental investigation of the transonic-flow-generation and shock-wave-reflection characteristics of a two-dimensional wind tunnel with 17-percent-open perforated walls (National Advisory Committee for Aeronautics, 1954), by Don D. Davis, George M. Stokes, Thomas B. Sellers, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
- The development of an 8-inch by 8-inch slotted tunnel for Mach numbers up to 1.28 (National Advisory Committee for Aeronautics, 1955), by B. H. Little, James M. Cubbage, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
- Transonic wind-tunnel investigation of the interference between a 45©� sweptback wing and a systematic series of four bodies (National Advisory Committee for Aeronautics, 1952), by Donald L. Loving, Dewey E. Wornom, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
- Transonic wind-tunnel investigation of an unswept wing in combination with a systematic series of four bodies (National Advisory Committee for Aeronautics, 1953), by Bruce B. Estabrooks, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (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). ([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)
- 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 ([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 ([U.S. G.P.O.], 1949), by United States House Committee on Armed Services (page images at HathiTrust)
- Fundamental studies of subsonic and transonic flow separation. Part I. First phase summary report (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), by Zhengming 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, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
- An Investigation of three-dimensional wall interference in a variable porosity transonice wind tunnel (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1974., 1974), by Travis W. Binion, United States. Air Force. Arnold Air Force Base, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
- Application of linearized transonic theory to tunnel blockage interference (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1974., 1974), by C. F. Lo, United States. Air Force. Arnold Air Force Base, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
- A study of acoustic disturbances and means of suppression in ventilated transonic wind tunnel walls (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977., 1977), by N. Sam Dougherty, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (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 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1978., 1978), by Jimmy Walker, Sverdrup Corporation, United States. Naval Air Systems Command, and Arnold Engineering Development Center (page images at HathiTrust)
- The effect of plenum volume on the test section flow characteristics of a perforated wall transonic tunnel (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1970., 1970), by C. F. Anderson, O. P. Credle, A. Anderson, Arnold Engineering Development Center, United States. Air Force. Systems Command, 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 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1962., 1962), by J. E. Robertson, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
- Perforated wall noise in the AEDC-PWT 16-ft and 4-ft transonic tunnels (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), by O. P. Credle, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
- Calibration of the AEDC-PWT 16-ft transonic tunnel with the propulsion test section at various Reynolds numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), by F. M. Jackson, United States. Air Force. Systems Command, 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 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1979., 1979), by F. M. Jackson, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
- Aerodynamic characteristics of perforated walls for transonic wind tunnels (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977., 1977), by J. L. Jacocks, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
- Experiments to assess the influence of changes in the tunnel wall boundary layer on transonic wall crossflow characteristics (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), by R. F. Starr, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
- Noise generation in transonic wind tunnels (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), by M. O. Varner, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
- Calculation of the boundary-layer growth in a Ludwieg tube (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), by James C. Sivells, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
- Tests of the ONERA calibration models in three transonic wind tunnels (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), by Travis W. Binion, United States. Air Force. Systems Command, Arnold Engineering Development Center, France. Office national d'études et de recherches aérospatiales, and Inc ARO (page images at HathiTrust)
- Fundamental studies of subsonic and transonic flow separation. Part III. Third phase summary report (Tullahoma, Tennessee : The University of Tennesse Space Institute, Gas Dynamics Division, 1979., 1979), by Zhengming Wu, Arnold Engineering Development Center, and University of Tennessee (System). Space Institute (page images at HathiTrust)
- Experimental uncertainty and drag measurements in the national transonic facility (National Aeronautics and Space Administration, Langley Research Center, 1994), by Stephen M. Batill and Langley Research Center (page images at HathiTrust)
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