Mach 6 Integrated Systems Testing for the Hypersonic Tunnel Facility
Author : Mark R. Wolke
Publisher :
Page : pages
File Size : 17,82 MB
Release : 2000
Category :
ISBN :
Author : Mark R. Wolke
Publisher :
Page : pages
File Size : 17,82 MB
Release : 2000
Category :
ISBN :
Author :
Publisher :
Page : 16 pages
File Size : 15,99 MB
Release : 1996
Category :
ISBN :
Author : Frank K. Lu
Publisher : AIAA
Page : 694 pages
File Size : 24,67 MB
Release : 2002
Category : Aerodynamics, Hypersonic
ISBN : 9781600864483
Author : Paul Czysz
Publisher :
Page : 116 pages
File Size : 46,91 MB
Release : 1963
Category : Hypersonic wind tunnels
ISBN :
The High Temperature Gas Dynamics Facility was developed as a result of the Aeronautical Systems Division's effort to extend the state-of the-art in hypersonic aerodynamic simulation. The facility is a hypersonic wind tunnel supplied with high pressure air, heated from a zirconia dioxide pebble heater. The maximum stagnation pressure and temperature is 40 atres and 4700 R, respectively. This facility is one of four of its kind in this hemisphere and the only Air Force facility of its type. This report discusses the modification of the facility to a two foot diameter test section with a Mach number range of 6 through 14 and its expected performance. This facility is scheduled to be operational in the Fall of 1963.
Author : Mark A. Woodling
Publisher :
Page : 20 pages
File Size : 33,11 MB
Release : 2000
Category :
ISBN :
Author : United States. Office of Science and Technology Policy
Publisher :
Page : 692 pages
File Size : 40,1 MB
Release : 1982
Category : Aeronautics
ISBN :
Author : United States. Office of Science and Technology Policy
Publisher :
Page : 692 pages
File Size : 30,48 MB
Release : 1982
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 702 pages
File Size : 13,94 MB
Release : 1995
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 616 pages
File Size : 30,76 MB
Release : 2000
Category : Aerodynamics
ISBN :
Author : Richard R. Cullom
Publisher :
Page : 36 pages
File Size : 36,39 MB
Release : 1972
Category : Hypersonic wind tunnels
ISBN :