General velocity potential for slender pointed body of revolution oscillating periodically in supersonic uniform stream, presented; two types of bodies of revolution are examined to demonstrate how aerodynamic stability derivates may be varied by changing contour of body; "flaring" aft end of body is shown to increase lift, as well to increase aerodynamic damping moment of finless body.
Nonsteady supersonic flow about pointed bodies of revolution
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 18 , n 8
1951
Aufsatz (Zeitschrift)
Englisch
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