摘要
本文用实验方法研究了冷却气流在放入一倍模型涡轮叶片内通道的压力分布、冷热态阻力及局部换热系数分布。
In this paper the test results of Pressure distribution,resistance under heating and without heating flow fields,distribution of local heat transfer coefficient in the cooling passages ofa modeled gas turbine blade are presented.
出处
《工程热物理学报》
EI
CAS
CSCD
北大核心
1996年第3期323-327,共5页
Journal of Engineering Thermophysics