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AWT Aerodynamic Design StatusThe aerodynamic design of the NASA Altitude Wind Tunnel is presented in viewgraph format. The main topics covered are: analysis of a plenum evacuation system; airline definition and pressure loss code development; contraction geometry and code analysis; and design of the two stage fan. Flow characteristics such as pressure ratio, mach number distribution, adiabatic efficiency, and losses are shown.
Document ID
19920075367
Acquisition Source
Glenn Research Center
Document Type
Other
Authors
Davis, Milt W. (Sverdrup Technology, Inc. Saint Louis, MO, United States)
Date Acquired
August 15, 2013
Publication Date
March 20, 1984
Publication Information
Publication: Wind Tunnel Modeling Seminar
Subject Category
Aerodynamics
Research And Support Facilities (Air)
Meeting Information
Meeting: Wind Tunnel Modeling Seminar
Location: Cleveland, OH
Country: United States
Start Date: March 20, 1984
End Date: March 21, 1984
Sponsors: NASA Glenn Research Center
Accession Number
92N70491
Distribution Limits
Public
Copyright
Public Use Permitted.

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