Consideration of Dynamic Loads on the Vertical Tail by the Theory of Flat Yawing Maneuvers
Description:
"Dynamic yawing effects on vertical-tail loads are considered by a theory of flat yawing maneuvers. A comparison is shown between computed loads and the loads measured in flight on a fighter airplane. The dynamic effects were investigated on a large flying boat for both an abrupt rudder deflection and sinusoidal rudder deflection" (p. 91).
Date:
March 15, 1946
Creator:
Boshar, John & Davis, Philip
Item Type:
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Partner:
UNT Libraries Government Documents Department