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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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Numerical prediction of cooling performance sensitivity of 1st stage nozzle guide vane under aerothermal conditions
会议论文
ASME 2019 Gas Turbine India Conference, GTINDIA 2019, Chennai, Tamil Nadu, India, December 5, 2019 - December 6, 2019
Authors:
Prapamonthon P
;
Yin B(银波)
;
Yang GW(杨国伟)
;
Zhang MH(张莫晗)
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Submit date：2020/11/20
Aerothermal condition
Cooling effectiveness
Cooling performance
Thermal sensitivity
Turbine vane
