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The effects of scale and turbulence on the lift and drag of five airfoils, the N.A.C.A. 0006 , the N.A.C.A. 0021, the Clark Y, The U.S.A 35-A, and the U.S.N. P.S.6, hve been investigated in the Variable Density Wind Tunnel. Tests were made over a wide scale for only two different conditions of turbulence.

Report

United States. National Advisory Committee for Aeronautics

Published: 1938

Total Pages: 16


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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.