Serial/Series Title

Consideration of Dynamic Loads on the Vertical Tail by the Theory of Flat Yawing Maneuvers (open access)

Consideration of Dynamic Loads on the Vertical Tail by the Theory of Flat Yawing Maneuvers

"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
System: The UNT Digital Library