Publication Date:
2019-06-27
Description:
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.
Keywords:
PHYSICAL SCIENCES
Type:
LAR-11771
Format:
application/pdf
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