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西北工业大学 国内
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Flow and heat transfer characters in the integral internal cooling channel of a turbine blade
Tao Guo,
Huiren Zhu
, Zhixiang Zhou
Northwestern Polytechnical University Xian
Hunan Aviation Power Plant Research Institute
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探究 'Flow and heat transfer characters in the integral internal cooling channel of a turbine blade' 的科研主题。它们共同构成独一无二的指纹。
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Engineering
Airfoil Shape
33%
Blade Turbine
100%
Channel Model
33%
Cooling Channel
100%
Experimental Investigation
33%
Heat Transfer Coefficient
33%
Liquid Crystal
33%
Pressure Coefficient
33%
Pressure Drop
33%
Pressure Side
66%
Reynolds' Number
33%
Suction Side
66%
Thermochromic Liquid Crystal
33%
Trailing Edge
33%
Transients
33%