Experiments with a wing from which the boundary layer is removed by pressure or suction (1928)
NASA Technical Reports Server (NTRS) · leaf 16
N.A.O.A. Technical Memorandum No.473 Figs.1,2,3, CO Fig.l Compensating circulation with unsymmetrical vortex formation, r, circulation, ,velocity of parallel flow. Fig.3 Velocity values according to the Bernoulli equation. P, reaction pressure at exit of jet. w, exit velocity of air jets, v,… … Fig.4 Experimental apparatus.b, over-pressure in manometer
NASA Technical Reports Server (NTRS)
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