Book Description
A large scale, variable-geometry inlet system with a design Mach number of 3.0 was tested at Mach numbers from 0.6 to 1.28. Variable features for off-design operation are an adjustable-height ramp system and a translating cowl.
Author : Norman D. Wong
Publisher :
Page : 52 pages
File Size : 42,8 MB
Release : 1973
Category : Drag (Aerodynamics)
ISBN :
A large scale, variable-geometry inlet system with a design Mach number of 3.0 was tested at Mach numbers from 0.6 to 1.28. Variable features for off-design operation are an adjustable-height ramp system and a translating cowl.
Author : Warren E. Anderson
Publisher :
Page : 68 pages
File Size : 30,21 MB
Release : 1970
Category : Jet engines
ISBN :
Author :
Publisher :
Page : 520 pages
File Size : 18,16 MB
Release : 1974
Category :
ISBN :
Author :
Publisher :
Page : 1570 pages
File Size : 18,83 MB
Release : 1974
Category : Government publications
ISBN :
Author :
Publisher :
Page : 104 pages
File Size : 17,14 MB
Release : 1980
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 464 pages
File Size : 41,72 MB
Release : 1995
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 442 pages
File Size : 13,2 MB
Release : 1989
Category : Airplanes
ISBN :
Author : United States. Superintendent of Documents
Publisher :
Page : 1408 pages
File Size : 25,88 MB
Release : 1976
Category : United States
ISBN :
Author : Mark R. Nichols
Publisher :
Page : 100 pages
File Size : 43,70 MB
Release : 1980
Category : Aerodynamics
ISBN :
Author :
Publisher :
Page : 100 pages
File Size : 32,70 MB
Release : 1980
Category :
ISBN :