Results 71 to 80 of about 101,352 (285)
Pressure Response in Supersonic Wind-Tunnel Pressure Instrumentation [PDF]
Journal of Applied Physics, 1953 In the development of high-speed aircraft, rockets, missles, etc., wind-tunnel pressure measurements at supersonic velocities are necessary to determine certain aerodynamic characteristics. Because of the lack of knowledge concerning the proper choice of parameters in the design of pressure instrumentation, the response time has been known to exceed ...
openaire +3 more sources
Journal of Aerospace Technology and Management, 2011 The Pilot Transonic Wind Tunnel of Institute of Aeronautics and Space (PTT Pilot Transonic Wind Tunnel) is an important result of a tremendous effort to install a high speed wind tunnel complex (TTS ...
João Batista P Falcão Filho +2 more
doaj
Streamline curvature design procedure for subsonic and transonic ducts [PDF]
A procedure for designing ducts for subsonic and transonic speeds is described. Examples discussed are a wind-tunnel contraction cone, a supersonic nozzle, and a diffuser. A listing of the computer program is included.
Barger, R. L.
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, 1982 An improved test section for a supersonic or hypersonic wind tunnel is disclosed wherein the model tested is shielded from the noise normally radiated by the turbulent tunnel wall boundary layer.
Beckwith, I. E., Creel, T. R., Jr.
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Utilizing Modal Testing for Monitoring the Structural Health of Wind Tunnel Facility Hardware [PDF]
The 10- by 10-Foot Abe Silverstein Supersonic Wind Tunnel (1010) is the largest and fastest wind tunnel facility at NASAs Glenn Research Center(GRC) and is specifically designed to test supersonic propulsion components from inlets and nozzles to full ...
Pederson, Kenneth, Suarez, Vicente
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Low-disturbance wind tunnels [PDF]
During the past years, there was an extensive program under way at the Langley Research Center to upgrade the flow quality in several of the large wind tunnels. This effort has resulted in significant improvements in flow quality in these tunnels and has
Applin, Z. T. +3 more
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Discussion: “Supersonic Diffusers for Wind Tunnels” (Neumann, E. P., and Lustwerk, F., 1949, ASME J. Appl. Mech., 16, pp. 195–202) [PDF]
, 1949 J. H. Keenan
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Supersonic turbulent separation tests in the Marshall Space Flight Center 7 in tunnel [PDF]
Supersonic wind tunnel test program on turbulent flow ...
Lowson, M. V.
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Investigations for Supersonic Transports at Transonic and Supersonic Conditions [PDF]
Several computational studies were conducted as part of NASA s High Speed Research Program. Results of turbulence model comparisons from two studies on supersonic transport configurations performed during the NASA High-Speed Research program are given ...
Owens, Lewis R. +2 more
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Wind tunnel evaluation of YF-12 inlet response to internal airflow disturbances with and without control [PDF]
, 1978 The response of terminal-shock position and static pressures in the subsonic duct of a YF-12 aircraft flight-hardware inlet to perturbations in simulated engine corrected airflow were obtained with and without inlet control.
Cole, G. L. +2 more
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