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Showing 1 to 1 of 1 for “"Flow Unstediness"”.
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Advancing Exhaust Flow Uniformity, Operational Stability, and Total Pressure Gain of Rotating Detonation Engines for Successful Turbine Integration
… a shock-laden, highly unsteady exhaust flow field that differs substantially from steady, subsonic flow required at the turbine inlet.This dissertation aims to develop novel RDC designs with tailored inlet and exit geometries for successful turbine integration. Firstly, RDC exit was …