Wind tunnel tests to improve static directional stability of unswept-wing aircraft at mach 0.8-2.2
WIND-TUNNEL INVESTIGATION OF DEVICES TO IMPROVE STATIC DIRECTIONAL STABILITY OF AN UNSWEPT-WING AIRPLANE MODEL AT MACH NUMBERS FROM 0.8 TO 2.2
01.12.1958
Sonstige
Keine Angabe
Englisch
Engineering Index Backfile | 1960
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