The Static Stability Characteristics of Several Cone-cylinder-flare-cylinder Configurations at Mach Numbers 0.4 to 4.5

The Static Stability Characteristics of Several Cone-cylinder-flare-cylinder Configurations at Mach Numbers 0.4 to 4.5
Author: D. J. Spring
Publisher:
Total Pages: 270
Release: 1963
Genre:
ISBN:

Download The Static Stability Characteristics of Several Cone-cylinder-flare-cylinder Configurations at Mach Numbers 0.4 to 4.5 Book in PDF, Epub and Kindle

The aerodynamic characteristics of various cone cylinder-flare-skirt configurations were inves tigated between Mach Numbers 0.4 to 4.5. The Reynolds number range for the tests was from 0.5 to 6.0 million per foot. Data are presented in basic form, along with cross plots, to show the effect of changing various body component shapes. (Author).


The Static Stability Characteristics of Several Cone-cylinder-flare-cylinder Configurations at Mach Numbers 0.4 to 4.5
Language: en
Pages: 270
Authors: D. J. Spring
Categories:
Type: BOOK - Published: 1963 - Publisher:

GET EBOOK

The aerodynamic characteristics of various cone cylinder-flare-skirt configurations were inves tigated between Mach Numbers 0.4 to 4.5. The Reynolds number rang
Effect of Jet Pluming on the Static Stability of Cone-cylinder-flare Configurations as a Mach Number of 9.65
Language: en
Pages: 86
Authors: William F. Hinson
Categories: Fluid mechanics
Type: BOOK - Published: 1962 - Publisher:

GET EBOOK

Index of NASA Technical Publications
Language: en
Pages: 448
Authors: United States. National Aeronautics and Space Administration
Categories: Aeronautics
Type: BOOK - Published: 1960 - Publisher:

GET EBOOK

Technical Abstract Bulletin
Language: en
Pages: 1766
Authors: Defense Documentation Center (U.S.)
Categories: Technology
Type: BOOK - Published: 1961-07 - Publisher:

GET EBOOK