Longitudinal aerodynamic characteristics of nose cylinder-flare reentry bodies measured in hypersonic wind tunnel
A parametric study of the aerodynamic charac- teristics of nose-cylinder-flare bodies at a mach number of 6.0
1965-06-01
Miscellaneous
No indication
English
Hammerhead and Nose-Cylinder-Flare Aeroelastic Stability Revisited
Online Contents | 1995
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