NASA NTRS · 19920075367
AWT Aerodynamic Design Status
Abstract
The 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.
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Davis, Milt W.. 1984-03-20. AWT Aerodynamic Design Status. https://ntrs.nasa.gov/citations/19920075367
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