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The Altitude Wind Tunnel (AWT): A unique facility for propulsion system and adverse weather testingA 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.
Document ID
19850009758
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chamberlin, R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1985
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA PAPER 85-0314
NASA-TM-86921
NAS 1.15:86921
E-2415
Meeting Information
Meeting: Aerospace Sci. Meeting
Location: Reno, NV
Country: United States
Start Date: January 14, 1985
End Date: January 17, 1985
Sponsors: AIAA
Accession Number
85N18067
Funding Number(s)
PROJECT: RTOP 505-40-74
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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