Experimental investigation on impingement/effusion cooling with short normal injection holes

Xiao-Ming Tan1, Jingzhou Zhang2,1, Xu Huasheng3
1College of Energy and Power Engineering, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
2Collaborative Innovation Center of Advanced Aero-Engine, Beijing 100191, China
3China Gas Turbine Establishment, Aviation Industry Corporation of China, Chengdu 610500, China

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