Abstract
A numerical investigation is focused on the effect of bleed on the three-dimensional turbulent interaction generated by a sharp fin at Mach 3. For an incipiently separated configuration (8 deg fin, Re δ =5.6X10 5 ), 23% suction is applied over a rectangular area beneath the inviscid shock.
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Schedule a callMore From: AIAA journal. American Institute of Aeronautics and Astronautics
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