Transonic Performance of Ejector Nozzles Having Zero Boattail Angle and an Internal Base
Author :
Publisher :
Page : 124 pages
File Size : 30,25 MB
Release : 1965
Category :
ISBN :
NASA Technical Note
Author :
Publisher :
Page : 826 pages
File Size : 22,62 MB
Release : 1975
Category :
ISBN :
Book Description
Effect of Jet Velocity and Axial Location of Nozzle Exit on the Performance of a Twin-jet Afterbody Model at Mach Numbers Up to 2.2
Author : Bobbly Lee Berrier
Publisher :
Page : 84 pages
File Size : 30,20 MB
Release : 1969
Category : Drag (Aerodynamics)
ISBN :
Book Description
NASA Technical Memorandum
Author :
Publisher :
Page : 104 pages
File Size : 20,72 MB
Release : 1980
Category : Aeronautics
ISBN :
Book Description
Transonic Performance of a Convergent- Divergent Ejector Nozzle Designed for a Corrected Secondary-weight-flow Ratio of 0.07
Author :
Publisher :
Page : 38 pages
File Size : 39,2 MB
Release : 1964
Category :
ISBN :
Book Description
Summary of Research on Jet Exit Installations
Author :
Publisher :
Page : 28 pages
File Size : 36,14 MB
Release : 1966
Category :
ISBN :
Book Description
Data Base for the Prediction of Airframe/propulsion System Interference Effects
Author :
Publisher :
Page : 444 pages
File Size : 22,61 MB
Release : 1979
Category :
ISBN :
Book Description
Bibliography on Aerodynamics of Airframe/engine Integration of High-speed Turbine-powered Aircraft
Author : Mark R. Nichols
Publisher :
Page : 100 pages
File Size : 27,84 MB
Release : 1980
Category : Aerodynamics
ISBN :
Book Description
Two-dimensional Converging-diverging Rippled Nozzles at Transonic Speeds
Author : John R. Carlson
Publisher :
Page : 116 pages
File Size : 48,93 MB
Release : 1994
Category : Aerodynamics
ISBN :
Book Description
NASA Reference Publication
Author :
Publisher :
Page : 116 pages
File Size : 31,25 MB
Release : 1977
Category : Astronautics
ISBN :
