An analysis was made to determine the effect of rolling pull-out maneuvers on the wing and aileron loads of a typical fighter airplane, the P- 47B. The results obtained indicate that higher loads are imposed upon wings and ailerons because of the rolling pull-out maneuver, than would be obtained by application of the loading requirements to which the airplane was designed. An increase of 102 lb or 15 percent of wing weight would be required if the wing were designed for rolling pull-out maneuver. It was also determined that the requirements by which the aileron was originally designed were inadequate.
Analysis of the effect of rolling pull-outs on the wing and aileron loads of a fighter airplane
1945
83 pages
Report
No indication
English
Aerodynamics , Aircraft , Flight loads , Wings , Ailerons , Loading(Handling) , Fighter aircraft , Requirements , Weight , Ati-16431 , Ati collection
Analysis of effect of rolling pull-outs on wing and aileron loads of fighter airplane
Engineering Index Backfile | 1946
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Engineering Index Backfile | 1944
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