High-fidelity simulations of a high-pressure turbine vane subject to large disturbances: effect of exit Mach number on losses
Published in Journal of Turbomachinery, 2021
Recommended citation: Y. Zhao*, R. D. Sandberg. (2021). "High-fidelity simulations of a high-pressure turbine vane subject to large disturbances: effect of exit Mach number on losses." Journal of Turbomachinery, 143, 091002.
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