Effect of nose bluntness, fineness ratio, cone angle, and model base on aerodynamic characteristics of blunt bodies
Effects of Nose Bluntness, Fineness Ratio, Cone Angle, and Model Base on the Static Aerodynamic Characteristics of Blunt Bodies at Mach Numbers of 1.57, 1.80, and 2.16 and Angles of Attack up to 180 Deg
1963-05-01
Miscellaneous
No indication
English
Engineering Index Backfile | 1961
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