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DRAG CHARACTERISTICS OF PLATES, CONES AND SPHERES IN THE WAKE OF A CYLINDRICAL BODY AT TRANSONIC SPEEDS,
Final rept. Feb 60-Aug 63,
MINNESOTA UNIV MINNEAPOLIS DEPT OF AERONAUTICS AND ENGINEERING MECHANICS
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The drag coefficients of a circular flat plate, 45 degree half-angle cone, sphere and guide surface parachute model have been measured in the wake of a simulated ogive cylinder at transonic speeds. Stagnation and base pressure measurements were also made. The Mach number range was from 0.85 to 1.2 and secondary body size and position in the wake were selected parameters. Author
APPROVED FOR PUBLIC RELEASE