CHANNELED BODIES STREAMLINED WITH FLAT AND CONIC SHOCK WAVES,
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
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Consideration is given to examples of precise solutions for external flow around channeled bodies with supersonic velocities at the inlet to the internal channel, and the corresponding coefficients are calculated. Two classes of bodies are investigated 1 bodies consisting of flat faces and streamlined over the design regime with the formation of flat, attached shock waves, 2 axisymmetric bodies for which external flow is conic.