The roll-damping derivative is one of the many aerodynamic coefficients that influence the flight dynamics of a rolling missile. At present, the knowledge of this derivative is limited, especially for unfinned bodies of revolution in hypersonic flight. This note presents a quick method of approximating the hypersonic roll-damping derivative of a slight blunted cone. (Author)
Blunt-Cone Roll-Damping Derivative
1968
7 pages
Report
No indication
English
Blunt-cone roll-damping derivative.
AIAA | 1969
|Blunt cone laminar friction drag.
AIAA | 1966
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