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As a passive flow control device, bleed system is applied to supersonic inlet to imrpove flow quality and flow stability (inlet buzz). An enhanced bleed boundary condition is developed, and multi-point design optimization is carried to obtain bleed conditions for supersonic inlet in a wide range of operating conditions.

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This page is a summary of: Effects of Optimized Bleed System on Supersonic Inlet Performance and Buzz, Journal of Propulsion and Power, March 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b37474.
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