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The variation with Reynolds number of pressure distribution over an airfoil section (1938)
NASA Technical Reports Server (NTRS) · leaf 7
REPORT NO. 613—NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS … (a) Effective Eeynolds Number, 430,000. (o) Effective Reynolds Kumber, 3,100,000. (b) Effective Eeynolds Number, 1,800,000. (d) Effective Reynolds Number, 8,200,000. Fiocbi 6.—Pressure-distribution diagrams showing the spread of separation at fonr values of tbe Reynolds Number.NASA Technical Reports Server (NTRS)
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