System consists of movable auxiliary aerodynamic sensors mounted on fuselage and connected to trailing-edge flaps by rigid mechanical linkages. System achieves alleviation by reducing lift-curve slope of airplane to such a small value that gust-induced angles of attack will result in small changes in lift.
Gust alleviation system to improve ride comfort of light airplanes
1975-10-01
Sonstige
Keine Angabe
Englisch
SAE Technical Papers | 1975
|Analysis of gust-alleviation system for transport airplanes
Engineering Index Backfile | 1964
|NTRS | 1971
|SAE Technical Papers | 1937
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