An Investigation of a Supersonic Wind Tunnel Diffuser
Author : John P. Hartin
Publisher :
Page : 72 pages
File Size : 38,5 MB
Release : 1960
Category : Wind tunnels
ISBN :
Author : John P. Hartin
Publisher :
Page : 72 pages
File Size : 38,5 MB
Release : 1960
Category : Wind tunnels
ISBN :
Author : James Parker Sturrock
Publisher :
Page : 92 pages
File Size : 49,87 MB
Release : 1948
Category : Wind tunnels
ISBN :
Author : Klaus Oswatitsch
Publisher :
Page : 30 pages
File Size : 22,55 MB
Release : 1948
Category : Diffusers
ISBN :
Author : J. L. Diggins
Publisher :
Page : 22 pages
File Size : 49,61 MB
Release : 1951
Category :
ISBN :
Author : Francis M. Jackson
Publisher :
Page : 70 pages
File Size : 49,6 MB
Release : 1968
Category :
ISBN :
Author : Angus Nathaniel MacDonald
Publisher :
Page : 144 pages
File Size : 10,56 MB
Release : 1947
Category :
ISBN :
Author : Heinrich Ramm
Publisher :
Page : 34 pages
File Size : 23,25 MB
Release : 1947
Category : Supersonic diffusers
ISBN :
Author : Arthur Kantrowitz
Publisher :
Page : 38 pages
File Size : 29,21 MB
Release : 1945
Category : Aerodynamics, Supersonic
ISBN :
Summary: The deceleration of air from supersonic velocities in channels has been studied. It has become apparent that a normal shock in the diverging part of the diffuser is probably necessary for stable flow, and ways of minimizing the intensity of this shock have been developed. The effect of various geometrical parameters, especially contraction ratio in the entrance region, on the performance of supersonic diffusers has been investigated. By the use of these results, diffusers were designed which, starting without initial boundary layer, recovered 90 percent of the kinetic energy in supersonic air streams up to a Mach number of 1.85.
Author : Patrick J. Johnston
Publisher :
Page : 24 pages
File Size : 37,68 MB
Release : 1960
Category : Mach number
ISBN :
Author : John K. Molloy
Publisher :
Page : 36 pages
File Size : 49,28 MB
Release : 1971
Category : Aerodynamics, Supersonic
ISBN :