Numerical Investigation of Loss Development in a Low-Pressure Turbine Cascade With Unsteady Inflow and Varying Inlet Endwall Boundary Layer

Numerical Investigation of Loss Development in a Low-Pressure Turbine Cascade With Unsteady Inflow and Varying Inlet Endwall Boundary Layer
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具有不稳定流入和变化入口端壁边界层的低压涡轮叶栅损失发展的数值研究

DOI:
10.1115/gt2021-59606
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发表时间:
2021
期刊:
Volume 2B: Turbomachinery — Axial Flow Turbine Aerodynamics; Deposition, Erosion, Fouling, and Icing
影响因子:
--
通讯作者:
Niehuis
Niehuis
中科院分区:
--
文献类型:
--
作者:
Schubert;Niehuis

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