Discussion of the results of the boundary-layer tests of an airfoil fitted with a rotary cylinder (1927)
NASA Technical Reports Server (NTRS) · leaf 13
Fig.3 N.A.C.A. Technical Memorandum No.424 … V,m/a V, Velocity ij, Distance from surface JSl-W, Measuring points (See section 3) Velocity distribution with cylinder at rest and Fig.3 s'ap closGd (0) • (Reproduction of Fig.5 of T.M.411)
NASA Technical Reports Server (NTRS)
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