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Experimental investigation of the effects of support interference on the drag of bodies of revolution at a Mach number of 1.5
Testing was conducting to evaluate the effects of support interference on the drag characteristics of two bodies of revolution at zero angle of attack at Mach number 1.5. Drag and base-pressure measurements are made for a variety of Reynolds numbers to determine the effect of varying the length or diameter of the rear support.
Date:
May 7, 1948
Creator:
Perkins, Edward W.
System:
The UNT Digital Library