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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
Langley Research Center
Document Type
Conference Paper
Authors
Bret A Marks (McDonnel Aircraft (United States) St Louis, United States)
David E Hahne (Langley Research Center Hampton, United States)
Date Acquired
August 14, 2013
Publication Date
April 1, 1990
Publication Information
Publication: Aerodynamics of Combat Aircraft Controls and of Ground Effects
Publisher: North Atlantic Treaty Organization
ISBN: 92-835-0555-7
Subject Category
Aircraft Stability And Control
Meeting Information
Meeting: Symposium of the fluid Dynamics Panel
Location: Madrid
Country: US
Start Date: October 2, 1989
End Date: October 5, 1989
Sponsors: North Atlantic Treaty Organization
Accession Number
90N28521
Distribution Limits
Public
Copyright
Other
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