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.
Experimental Investigation of a Large-scale, Two-dimensional, Mixed-compression Inlet System
Author : Norman D. Wong
Publisher :
Page : 52 pages
File Size : 33,33 MB
Release : 1973
Category : Drag (Aerodynamics)
ISBN :
