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Multi-step optimization strategy to improve the aerodynamic performance of axial turbines operating at high Mach number unsteady flow.
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This page is a summary of: Three Dimensional Optimization for Subsonic Axial Turbines Operating at High Unsteady Inlet Mach Number, July 2018, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2018-4480.
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