Flow Quality and Operational Enhancements in the NASA Lewis 8- by 6-Foot Supersonic Wind Tunnel
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Page : 20 pages
File Size : 20,93 MB
Release : 1998
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Page : 20 pages
File Size : 20,93 MB
Release : 1998
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Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 56 pages
File Size : 42,2 MB
Release : 2018-07-10
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ISBN : 9781722655525
The 8- by 6-Foot Supersonic Wind Tunnel (SWT) at Lewis Research Center is available for use by qualified researchers. This manual contains tunnel performance maps which show the range of total temperature, total pressure, static pressure, dynamic pressure, altitude, Reynolds number, and mass flow as a function of test section Mach number. These maps are applicable for both the aerodynamic and propulsion cycle. The 8- by 6-Foot Supersonic Wind Tunnel is an atmospheric facility with a test section Mach number range from 0.36 to 2.0. General support systems (air systems, hydraulic system, hydrogen system, infrared system, laser system, laser sheet system, and schlieren system are also described as are instrumentation and data processing and acquisition systems. Pretest meeting formats are outlined. Tunnel user responsibility and personal safety requirements are also stated. Soeder, Ronald H. Glenn Research Center...
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Page : 42 pages
File Size : 18,35 MB
Release : 1998
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Page : 16 pages
File Size : 17,76 MB
Release : 1998
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Author : E. Allen Arrington
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Page : 86 pages
File Size : 30,97 MB
Release : 1997
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Page : 20 pages
File Size : 38,89 MB
Release : 1996
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Author : E. Allen Arrington
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Page : 24 pages
File Size : 37,20 MB
Release : 1995
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Page : 38 pages
File Size : 18,46 MB
Release : 1998
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Page : 392 pages
File Size : 30,71 MB
Release : 1998
Category : Aerodynamics
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Page : 1154 pages
File Size : 22,30 MB
Release : 1999-07
Category : Government publications
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