NASA NTRS · 19900019205
Innovative control concepts and component integration for a generic supercruise fighter
Abstract
The 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.
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Marks, Bret A., Hahne, David E.. 1990-04-01. Innovative control concepts and component integration for a generic supercruise fighter. https://ntrs.nasa.gov/citations/19900019205
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