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Airfoil Theory at Supersonic Speed (1939)
NASA Technical Reports Server (NTRS) · leaf 58
N.A.C.A. Technical Memorandum Ho. 897 Pigs. 11,18,13,14 __ Figure 12.- Trapesoidal wing with constant lift distribution. Induced downwash velocity in section CO (at right angles to flow direction) (tanT«l/V5; tand-V3). Figure 11.- Trapesoidal wing with constant lift distribution. Induced downwash… … Figure 13.- Trapesoidal wing with constant lift distribution. Profile sections. (tanoC = V3; tanT = 1/V5).NASA Technical Reports Server (NTRS)
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