期刊：Journal of Thermophysics and Heat Transfer [American Institute of Aeronautics and Astronautics] 日期：2021-04-01卷期号：35 (2): 210-224被引量：4
标识
DOI：10.2514/1.t6093
摘要
Numerical simulations are carried out to predict the phantom cooling on the blade tip and casing from blade-surface film coolant. The impacts of hole compound angles and shape for the pressure side...
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(2025-6-4)
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