Author : John Stack
Publisher : Unknown
Page : 70 pages
File Size : 48,9 Mb
Release : 1931
Category : Aerofoils
ISBN : UOM:39015095014976
Tests in the Variable Density Wind Tunnel to Investigate the Effects of Scale and Turbulence on Airfoil Characteristics by John Stack Pdf
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.