Determination of the Profile Drag of an Airplane Wing in Flight at High Reynolds Numbers (1939)
NASA Technical Reports Server (NTRS) · leaf 7
REPORT NO. 667—NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS I … Figure 4.—Boundary-layer-tube rack? mounted on wing. transition point on the smooth wing were made at The ratio of the dynamic pressure in the boundary Reynolds Numbers of 11,000,000 and 14,000,000, corre- layer close to the wing surface to the dynamic pressure sponding to lift coefficients of 0.34…
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