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Heat Transfer Research

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ISSN Печать: 1064-2285

ISSN Онлайн: 2162-6561

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GEOMETRIC-PARAMETER INFLUENCES ON AND ORTHOGONAL EVALUATION OF THERMOMECHANICAL PERFORMANCES OF A LAMINATED COOLING STRUCTURE

Том 51, Выпуск 1, 2020, pp. 57-82
DOI: 10.1615/HeatTransRes.2019030676
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Краткое описание

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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ЦИТИРОВАНО В
  1. Wang Chen, Zhang Jingzhou, Wang Chunhua, Tan Xiaoming, Multi-optimization of a specific laminated cooling structure for overall cooling effectiveness and pressure drop, Numerical Heat Transfer, Part A: Applications, 79, 3, 2021. Crossref

  2. Wang Chen, Wang Chunhua, Zhang Jingzhou, Cervone Angelo, Parametric Studies of Laminated Cooling Configurations: Overall Cooling Effectiveness, International Journal of Aerospace Engineering, 2021, 2021. Crossref

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