An Experimental Investigation of Steady Asymmetric Vortex Shedding from a Slender Body of Revolution at High Angles of Attack
AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH SCHOOL OF ENGINEERING
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An experimental investigation of the effects of Mach number and Reynolds number on the side forces induced on a slender body of revolution at high angles of attack was conducted. The tests were carried out in the Air Force Flight Dynamics Laboratorys Trisonic Gasdynamic Facility.