Experimental determination of the thickness of the boundary layer along a wing section (1932)
NASA Technical Reports Server (NTRS) · leaf 9
N.A.C.A. Technical Memorandum Ho. 679 Pigs. 3,4 0 35 85 135 cm 185 s ffig. 3 Pressxire distriljiition on upper side of wing. … .Hose s Pig* 4 Velocity distribution in boundary layer.
NASA Technical Reports Server (NTRS)
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