Comparison shown between computed loads and loads measured in flight on fighter airplane; dynamic effects investigated on large flying boat for both abrupt rudder deflection and sinusoidal rudder deflection; to take into account dynamic effects in design, specifications of yawing maneuverability or control movement are needed.
Consideration of dynamic loads on vertical tail by theory of flat yawing maneuvers
Nat Advisory Committee Aeronautics -- Tech Note
1946
12 pages
Supp sheets, Bibliography
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Consideration of dynamic loads on vertical tail by theory of flat yawing maneuvers
Engineering Index Backfile | 1946
|