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Innovative control concepts and component integration for a generic supercruise fighterThe results of a series of low speed wind tunnel tests conducted in the NASA Langley Research Center (LaRC) 12 ft Low Speed Wind Tunnel (LSWT) are highlighted. The main objectives of the tests were to provide generalized component integration guidelines and to investigate a variety of innovative control concepts designed to improve the high angle of attack (AOA) controllability of a generic class of supercruise fighters.
Document ID
19900019205
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Marks, Bret A. (McDonnell Aircraft Co. Saint Louis, MO., United States)
Hahne, David E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
April 1, 1990
Publication Information
Publication: AGARD, Aerodynamics of Combat Aircraft Controls and of Ground Effects
Subject Category
Aircraft Stability And Control
Accession Number
90N28521
Distribution Limits
Public
Copyright
Other
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