The resistance of a delta wing at small angle of attack in supersonic conical flow with its leading edges within the Mach cone is calculated by a method that separates out the suction force.
Resistance of a delta wing in a supersonic flow
1951-04-01
Miscellaneous
No indication
English
Resistance of Delta wing in supersonic flow
Engineering Index Backfile | 1951
|Resistance of a delta wing in a supersonic flow
TIBKAT | 1951
|Delta-wing configurations for supersonic transport
Engineering Index Backfile | 1963
|Supersonic Vortex Breakdown over a Delta Wing in Transonic Flow
British Library Conference Proceedings | 1993
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