Additional Results in a Free-flight Investigation of Control Effectiveness of Full-span, 0.2-chord Plain Ailerons at High Subsonic, Transonic, and Supersonic Speeds to Determine Some Effects of Wing Sweepback, Aspect Ratio, Taper, and Section Thickne
23.04.1948
Sonstige
Keine Angabe
Englisch
Engineering Index Backfile | 1950
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