Dynamic stability investigation of two right circular cylinders in axial free flight at Mach numbers from 0.4 to 1.7 fineness-ratio- 2.56 cylinder and fineness-ratio-4.0 cylinder with flared afterbody
Description: Dynamic longitudinal stability of right circular cylinders in axial free flight.
Date: February 28, 1957
Creator: Mc Fall, J. C., Jr.
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Partner: UNT Libraries Government Documents Department