The process of separation in the turbulent friction layer (1933)
NASA Technical Reports Server (NTRS) · leaf 11
N.A.C.A. Technical Memorandum Ho. 699 Tig. 1 … 010 2 4 6 8 10 12 y, mm Fig. 1 Velocity profiles on G-6'ttingen airfoil No. 387 (chord = 40 cm), flow velocity W0 = 30.8 m/s, angle of attack a = 12°, x = length of arc along suction side from foremost point (total length to trailing edge = 42.7 cm), y = distance from surface, w = velocity in…
NASA Technical Reports Server (NTRS)
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