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 : 16,90 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 : 10,51 MB
Release : 1947
Category : Airplanes
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 1370 pages
File Size : 38,10 MB
Release : 1949
Category : Aeronautics
ISBN :
Author : Donald H. Wood
Publisher :
Page : 204 pages
File Size : 23,56 MB
Release : 1934
Category : Aerofoils
ISBN :
Author :
Publisher :
Page : 420 pages
File Size : 47,76 MB
Release : 1927
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 424 pages
File Size : 27,66 MB
Release : 1927
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 508 pages
File Size : 15,56 MB
Release : 1926
Category : Aeronautics
ISBN :
Chiefly translations from foreign aeronautical journals.
Author : Fay Leone Faurote
Publisher :
Page : 424 pages
File Size : 31,42 MB
Release : 1927
Category : Aeronautics
ISBN :
Author : Harry Bernstein
Publisher :
Page : 686 pages
File Size : 31,6 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 : United States. Superintendent of Documents
Publisher :
Page : 2476 pages
File Size : 43,96 MB
Release : 1896
Category : Government publications
ISBN :