Effects of Wing Elasticity on the Aerodynamic Characteristics of a 45 Degree Sweptback-wing-fuselage Combination Measured in the Langley 8-foot Transonic Tunnel
1952-09-17
Sonstige
Keine Angabe
Englisch
Tests of 45° sweptback-wing model in Langley gust tunnel
Engineering Index Backfile | 1948
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