Abstract
We describe an analytical/numerical model representing the deflection and mixing of a single gaseous jet in supersonic crossflow. The jet cross section is modeled in terms of a compressible vortex pair that results from viscous and impulsive forces acting at the periphery of the jet. The behavior of the vortex pair is then combined with mass and momentum balances along the axis of the jet to form a model that describes the trajectory and mixing of the injected fluid
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Schedule a callMore From: AIAA journal. American Institute of Aeronautics and Astronautics
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