Calculation of the Load Distribution, at Supersonic Speeds, on a Sweptback Wing of Arbitrary Planform
1966
57 pages
Report
No indication
English
Aerodynamics , Aircraft , Load distribution , Supersonic flow , Sweptback wing , Wing loading , Computation , Computer , Digital , Distribution , Disturbance , Edge , Flow , Leading , Lift , Load , Loading , Speed , Subsonic , Supersonic , Sweepback , Trailing , Wake
Trim drag at supersonic speeds of various delta-planform configurations
Engineering Index Backfile | 1960
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