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 Effect of Rolling Pull-Outs on Wing and Aileron Loads of a Fighter Airplane
01.03.1946
Sonstige
Keine Angabe
Englisch
Aerodynamics , AIRFOILS - NACA 64-(A)06 - ORDINATES LOW-DRAG (BLOWER BLADE) , AIRFOILS - CASCADES , FLOW - VANES, GUIDE , AIRFOILS - NACA 65-410 - ORDINATES LOW-DRAG (BLOWER BLADE) , AIRFOILS - NACA 65-810 - ORDINATES LOW-DRAG (BLOWER BLADE) , CHARTS - VANES, GUIDE , AIRFOILS - NACA 65-210 - ORDINATES LOW-DRAG (BLOWER BLADE) , VANES, GUIDE , AIRFOILS - NACA 65-110 - ORDINATES LOW-DRAG (BLOWER BLADE) , AIRFOILS - NACA 65-(12)10 - ORDINATES LOW-DRAG (BLOWER BLADE)
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 | 1955
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