Effects of conical camber for triangular wing- body-tail combinations on aerodynamic characteristics
A Wind-Tunnel Investigation of the Effects of Conical Camber for an Airplane Configuration Having a Triangular Wing of Aspect Ratio 2.2
1957-04-30
Miscellaneous
No indication
English
Engineering Index Backfile | 1957
|Slender Delta Wing with Conical Camber
AIAA | 1974
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