Investigation of the Effects of Leading-edge Flaps on the Aerodynamic Characteristics in Pitch at Mach Numbers from 0.40 to 0.93 of a Wing-fuselage Configuration with a 45 Degree Sweptback Wing of Aspect Ratio 4
20.08.1953
Sonstige
Keine Angabe
Englisch
Engineering Index Backfile | 1960
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