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Gases bleeding from the base of a projectile are confirmed to yield drag reduction and hence, range extension. It is desired to define the geometric characteristics of bleed exit configuration that maximizes the drag reduction.
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This page is a summary of: Computational Parametric Study and Live Firing Validation of Base-Bleed Exit Configuration, Journal of Spacecraft and Rockets, November 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a35451.
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