Heat transfer performance optimization of turbine blade internal cooling channel with pin-fins and recessed-extruded endwalls

被引：0
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作者：
Do, Khanh-Duy Cong [1 ]
Chung, Duy-Hung [2 ]
Plourde, Frédéric [3 ]
Duong, Viet-Dung [4 ]
Pham, Gia-Diem [1 ]
Dinh, Cong-Truong [1 ]
机构：
[1] Department of Aerospace Engineering, School of Mechanical Engineering, Hanoi University of Science and Technology, Hanoi, Viet Nam
[2] Viettel Aerospace Institute, Hanoi, Viet Nam
[3] ENSMA, INSTITUT P’, UPR3346, Futuroscope Chasseneuil Cedex, France
[4] School of Aerospace Engineering, Vietnam National University, University of Engineering and Technology, Hanoi, Viet Nam
来源：
International Journal of Engine Research | 2024年
关键词：
1007.1 - 1101.2 - 1201.2 - 1301.1.2 - 201.5.2.2 - 206.1 - 301.1 - 302.2 - 306.1 - 408 Structural Design;
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摘要：
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