Dynamic yawing loads considered on basis of restricted theory; comparison shown between computed loads and load measured in flight on fighter airplane; in order 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 -- Report
1946
5 pages
Report
English
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Consideration of dynamic loads on vertical tail by theory of flat yawing maneuvers
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