Experimental Investigations of the Film Cooling Performance of a Micro-Tangential-Jet Scheme on a Gas Turbine Vane: Part 2—Heat Transfer Coefficient

Experimental Investigations of the Film Cooling Performance of a Micro-Tangential-Jet Scheme on a Gas Turbine Vane: Part 2—Heat Transfer Coefficient

مؤلف البحث
O Hassan, I Hassan
مجلة البحث
ASME 2012 International Mechanical Engineering Congress and Exposition
الناشر
American Society of Mechanical Engineers
تصنيف البحث
3
سنة البحث
2012