Static Longitudinal Stability of a Blunt-nosed Cylinder with Flared Afterbody at a Mach Number of 19.2

Static Longitudinal Stability of a Blunt-nosed Cylinder with Flared Afterbody at a Mach Number of 19.2
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Total Pages: 28
Release: 1965
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Static Longitudinal Stability of a Blunt-nosed Cylinder with Flared Afterbody at a Mach Number of 19.2
Language: en
Pages: 28
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:

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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
A Parametric Study of the Aerodynamic Characteristics of Nose-cylinder-flare Bodies at a Mach Number of 6.0
Language: en
Pages: 82
Authors: George C. Ashby
Categories: Aerodynamics, Hypersonic
Type: BOOK - Published: 1965 - Publisher:

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