The Altitude Wind Tunnel (AWT) - A unique facility for propulsion system and adverse weather testing
Author(s) -
R. Chamberlin
Publication year - 1985
Publication title -
23rd aerospace sciences meeting
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.1985-314
Subject(s) - propulsion , meteorology , adverse weather , aerospace engineering , environmental science , wind tunnel , aeronautics , computer science , engineering , physics
A need has arisen for a new wind tunnel facility with unique capabilities for testing propulsion systems and for conducting research in adverse weather conditions. New propulsion system concepts, new aircraft configurations with an unprecedented degree of propulsion system/aircraft integration, and requirements for aircraft operation in adverse weather dictate the need for a new test facility. Required capabilities include simulation of both altitude pressure and temperature, large size, full subsonic speed range, propulsion system operation, and weather simulation (i.e., icing, heavy rain). A cost effective rehabilitation of the NASA Lewis Research Center's Altitude Wind Tunnel (AWT) will provide a facility with all these capabilities.
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