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 … Figure 4.—Boundary-layer-tube racks mounted on wing. The ratio of the dynamic pressure in the boundary- transition point on the smooth wing were made at layer close to the wing surface to the dynamic pressure Reynolds Numbers of 11,000,000 and 14,000,000, corre- just outside the boundary layer was…
NASA Technical Reports Server (NTRS)
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