Determining the velocity distribution in the boundary layer of an airfoil fitted with a rotary cylinder (1927)
NASA Technical Reports Server (NTRS) · leaf 17
N.A.C.A- Toehni c al Memo randum No.411 Fig. 5 … V, Velocity ij, Distance from surface HI-ME, Measuring points (See section 3) Fig. 5 Velocity distribution with cylinder at rest and gap closed (C)•
NASA Technical Reports Server (NTRS)
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