Aerodynamic Performance and Static Stability Characteristics of a Blunt Nosed, Boattailed, 13 Deg Half Cone at Mach Numbers from 0.6 to 5.0

Aerodynamic Performance and Static Stability Characteristics of a Blunt Nosed, Boattailed, 13 Deg Half Cone at Mach Numbers from 0.6 to 5.0
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Total Pages: 76
Release: 1961
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A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0
Language: en
Pages: 20
Authors: Robert S. Osborne
Categories: Aerodynamics
Type: BOOK - Published: 1960 - Publisher:

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Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers of 5.2, 7.4, and 10.4
Language: en
Pages: 78
Static Stability Characteristics of Blunt Low-fineness-ratio Bodies of Revolution at a Mach Number of 24.5 in Helium
Language: en
Pages: 54
Authors: Robert D. Witcofski
Categories: Aerodynamics
Type: BOOK - Published: 1964 - Publisher:

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