An Application of Lifting-surface Theory to the Prediction of Angle-of-attack Hinge-moment Parameters for Aspect Ratio 4.5 Wings
01.09.1947
Sonstige
Keine Angabe
Englisch
AIRFOILS - NACA 0012-64 (MOD ) - TAIL SURFACE , LOAD DISTRIBUTION, WING-SPAN , LIFT DISTRIBUTION - WINGS , AIRFOILS - NACA 0009-0015 - LOW-DRAG (TAIL SURFACE) , AIRFOILS - NACA 65(216)-014 - LOW-DRAG (TAIL SURFACE) , AIRFOILS - ANGLE OF ATTACK , CONTROL SURFACES - HINGE MOMENTS , DOWNWASH , AIRFOILS - ASPECT RATIO , THEORIES - AIRFOILS - LIFTING-SURFACE
Engineering Index Backfile | 1947
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TIBKAT | 1957
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