Resistance of delta wing at small angle of attack in supersonic conical flow with its leading edges within Mach cone is calculated by method that separates out suction force. English abstract from Prikladnaya Matematika i Mekhanika n 4 1947 p 495-6.
Resistance of Delta wing in supersonic flow
Nat Advisory Committee Aeronautics -- Tech Memo
National Advisory Committee for Aeronautics -- Technical Memorandums ; 11 , Memo n 1283
1951
6 pages
Report
English
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