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Gust Alleviation for General Aviation Aircraft
ISSN: 0148-7191, e-ISSN: 2688-3627
Published October 01, 1996 by SAE International in United States
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This paper describes a preliminary research flight test program to investigate the development of a gust alleviation system for Commuter and General Aviation Aircraft. The program was conducted on a variable stability Navion aircraft and investigated the use of both up and down flap deflection in combination with elevator to alleviate the effects of gusts.
A second phase of the program to investigate methods of sensing gusts in sufficient time for use of this method is currently in the planning stage.
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