Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 878 pages
File Size : 11,77 MB
Release : 1957
Category : Aeronautics
ISBN :
Author : Davis H. Crawford
Publisher :
Page : 680 pages
File Size : 13,38 MB
Release : 1956
Category : Aeronautics
ISBN :
At the stagnation point, the theory of Sibulkin, using the diameter and conditions behind the normal shock, was in good agreement with the experiment when the velocity graident at the stagnation opint appropriate to the free-stream Mach number was used.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 580 pages
File Size : 27,42 MB
Release : 1956
Category : Aeronautics
ISBN :
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : 376 pages
File Size : 46,14 MB
Release : 1959
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 524 pages
File Size : 21,3 MB
Release : 1953
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 508 pages
File Size : 34,74 MB
Release : 1954
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 616 pages
File Size : 42,54 MB
Release : 1948
Category : Mechanics, Applied
ISBN :
Author :
Publisher :
Page : pages
File Size : 42,21 MB
Release : 1959
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 596 pages
File Size : 20,34 MB
Release : 1957
Category : Mechanical engineering
ISBN :
Author :
Publisher :
Page : 610 pages
File Size : 48,34 MB
Release : 1957
Category : Mechanics, Applied
ISBN :
