Determining the velocity distribution in the boundary layer of an airfoil fitted with a rotary cylinder (1927)
NASA Technical Reports Server (NTRS) · leaf 19
IT.A.O.A. Technical Memorandum No.411 Fig.? V, Velocity ij, Distance from surface HE-"HE, Measuring points (See section 3) 3, C, The observations are indicated by cross marks … Fig.7 Comparison of the velocity distribution on the surface of the model with cylinder p,t rest(B) and that with cylinder at rest and sap closed(c).
NASA Technical Reports Server (NTRS)
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