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涡轮冷却叶片气动与传热设计优化
引用本文:虞跨海,岳珠峰,杨茜. 涡轮冷却叶片气动与传热设计优化[J]. 计算力学学报, 2010, 27(2): 310-314
作者姓名:虞跨海  岳珠峰  杨茜
作者单位:1. 西北工业大学,力学与土木建筑学院,西安,710072;河南科技大学,规划与建筑工程学院,洛阳,471003
2. 西北工业大学,力学与土木建筑学院,西安,710072
3. 西北工业大学,材料学院,西安,710072
基金项目:国家自然科学基金(50375124,10472094);;863计划基金(2006AA04Z401);;高等学校学科创新引智计划(B07050)资助项目
摘    要:提出了航空发动机涡轮冷却叶片叶栅气动与传热自动优化方法,利用函数解析成型方法实现了冷却叶片几何模型的参数化与自动生成,可以建立任意冷却内腔数量的叶片模型;基于N-S方程实现叶片流体域与固体域的流-热耦合分析;采用KS函数方法将多目标优化问题转化为单目标函数进行优化,以总压损失、叶片最高温度和平均温度最小为优化目标进行了自动优化,改善了叶片性能。

关 键 词:涡轮冷却叶片  多目标优化  KS函数  参数化建模  流-热耦合  
收稿时间:2008-02-12

Aerodynamic and heat transfer design optimization for cooling turbine blade
YU Kua-hai,YUE Zhu-feng and Yang Xi. Aerodynamic and heat transfer design optimization for cooling turbine blade[J]. Chinese Journal of Computational Mechanics, 2010, 27(2): 310-314
Authors:YU Kua-hai  YUE Zhu-feng  Yang Xi
Affiliation:1.School of Mechanics Civil Engineering and Architecture/a>;Northwestern Polytechnical University/a>;Xi'an 710072/a>;China/a>;2.School of Planning and Archtectural Engineering/a>;Henan University of Science and Technology/a>;Luoyang 471003/a>;3.School of Material/a>;China
Abstract:This paper presents an automated computer aid design optimization program for aerodynamic and heat transfer optimization of 2D internal cooling gas turbine blades.Parametric geometry models were developed with analytic function methods.The suction surface and pressure surface are presented by a series of quintic splines,the leading edge geometry and the trailing edge geometry were represented by circular arc which helps to maintain a smooth geometry connection at the end points of the pressure side and the ...
Keywords:cooling turbine blade  multi-objective optimization  KS function  parametric design  coupled aero-thermal analysis  
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