Author : Raymond F. Anderson
Publisher :
Page : 36 pages
File Size : 38,25 MB
Release : 1931
Category : Aerofoils
ISBN :
This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 398, and U.S.A. 45 airfoils as obtained from tests made in the Variable Density Wind Tunnel. The results are given at both low and high Reynolds numbers to show scale effect and to provide data for use in airplane design.
Author : John Stack
Publisher :
Page : 556 pages
File Size : 49,5 MB
Release : 1931
Category : Aerofoils
ISBN :
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.
Author :
Publisher :
Page : 626 pages
File Size : 47,14 MB
Release :
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 616 pages
File Size : 31,64 MB
Release : 1949
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 732 pages
File Size : 32,95 MB
Release : 1931
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 664 pages
File Size : 27,88 MB
Release : 1949
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 80 pages
File Size : 39,81 MB
Release : 1945
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 1874 pages
File Size : 18,92 MB
Release : 1928
Category : Aeronautics, Military
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 120 pages
File Size : 18,57 MB
Release : 1945
Category : Aeronautics
ISBN :
Author : United States. Federal Power Commission
Publisher :
Page : 140 pages
File Size : 37,48 MB
Release : 1949
Category : Electric power-plants
ISBN :
