Book Description
This lecture concerns the combining effects in airplane wings so as to save some of the dead weight.
Author : K. Thalau
Publisher :
Page : 674 pages
File Size : 10,21 MB
Release : 1926
Category : Airplanes
ISBN :
This lecture concerns the combining effects in airplane wings so as to save some of the dead weight.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 48 pages
File Size : 24,31 MB
Release : 1947
Category : Airplanes
ISBN :
Author : Christopher J. Borland
Publisher :
Page : 195 pages
File Size : 36,35 MB
Release : 1966
Category :
ISBN :
Methods are proposed for calculating the distribution of aerodynamic loads due to mutual interference effects between wings and bodies. The methods fall into two ranges of applicability: linear, and nonlinear, with angle of attack. Applicability of the linear loads methods to aeroelastic calculations is discussed. A computer program is presented which may be used to calculate interference loads at subsonic Mach numbers on a configuration consisting of (1) a body of any varying elliptic cross section and camber distribution, and (2) a wing with straight leading and trailing edges of any sweep angle, twist distribution, and camber distribution, located above or below the body centerline. Extension to the supersonic case is indicated. Generally good agreement with experimental data is found. Nonlinear wing-body interference loads are also considered. Several possible methods of representing the separated flow about a wing-body combination are proposed, and analyzed by the slender body theory. Numerical procedures are outlined, and some comparisons with experimental data are made.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 1370 pages
File Size : 33,36 MB
Release : 1949
Category : Aeronautics
ISBN :
Author : Donald H. Wood
Publisher :
Page : 204 pages
File Size : 11,38 MB
Release : 1934
Category : Aerofoils
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 508 pages
File Size : 46,99 MB
Release : 1926
Category : Aeronautics
ISBN :
Chiefly translations from foreign aeronautical journals.
Author : United States. Superintendent of Documents
Publisher :
Page : 2476 pages
File Size : 50,94 MB
Release : 1896
Category : Government publications
ISBN :
Author : Harry Bernstein
Publisher :
Page : 686 pages
File Size : 23,15 MB
Release : 1953
Category : Air jets
ISBN :
A one-dimensional analysis of the results of the parallel-jet mixing encountered in the testing of engines in supersonic wind tunnels is reported. Equations were derived for determining the total pressure and Mach number behind the tunnel terminal shock. The method represents a simple procedure for determining these quantities while a tunnel is still in the design stage. A specific example of the method is included.
Author : John C. Houbolt
Publisher :
Page : 14 pages
File Size : 47,48 MB
Release : 1953
Category :
ISBN :
Author :
Publisher :
Page : 1248 pages
File Size : 24,73 MB
Release :
Category : Government publications
ISBN :