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Heat Transfer Research
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ISSN Print: 1064-2285
ISSN Online: 2162-6561

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Heat Transfer Research

DOI: 10.1615/HeatTransRes.2019030676
pages 57-82


Chen Wang
College of Energy and Power Engineering, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China
Jing-Zhou Zhang
College of Energy and Power Engineering, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China; Collaborative Innovation Center of Advanced Aero-Engine, Beij ing, 100191, China
Chun-hua Wang
College of Energy and Power Engineering, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Jun Ji
College of Energy and Power Engineering, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China
Xiao-Ming Tan
College of Energy and Power Engineering, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China


Numerical simulations are conducted to illustrate the geometric-parameter influences on and orthogonal evaluation of thermomechanical performances of a specific laminated cooling structure, under the representative engine-simulated environment. Five geometric parameters taken into consideration are the film-hole diameter, impinging-hole diameter, pin-fin diameter, streamwise hole-to-hole pitch, and the spanwise hole-to-hole pitch. Firstly, each geometric-parameter influence is investigated individually among its varying range while maintaining the other geometric parameters. Secondly, an orthogonal analysis (5-factors and 4-levels for each factor) is performed for evaluating the importance of each geometric-parameter on the thermomechanical performances of a laminated cooling structure, in the viewing of comprehensive performance index which is constructed by applying a weighted sum method, taking the overall cooling effectiveness, cooling air pressure drop, maximum thermal stress, and maximum thermal deformation into consideration. From the orthogonal analysis, a relatively optimum combination of the above geometric parameters is presented.


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