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模拟退火算法与响应面模型在压气机动叶优化设计中的应用 被引量:3

Application of a Simulated Annealing and Response Surface Model in Optimization Design of Moving Compressor Vanes
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摘要 开发了模拟退火算法与响应面方法相结合的具有全局寻优能力的优化程序,采用三维粘性流场求解程序进行流场求解,并对某型轴流压气机转子叶片进行了弯掠数值优化设计。结果表明,弯掠联合采用可以有效地改善流场内的流动状况,减少激波损失与尾迹损失,提高效率,表明了所用优化方法的可行性。 An optimization program with global optimization ability has been developed, which combines simulated annealing algorithm with response surface models. A solution of the flow field is being found by using the three dimensional viscous flow equations. The sweep and twist of a certain type of axial compressor blade are then optimally designed by numerical calculation. Results show that flowing conditions in the flow field can be improved effectively by combined sweep and twist, increasing the efficiency by reducing losses caused by shock waves and wakes. This optimization design method is feasible. Figs 6, table 1 and refs 6.
出处 《动力工程》 EI CSCD 北大核心 2006年第4期483-485,524,共4页 Power Engineering
基金 高校博士点基金项目(20030213022)
关键词 动力机械工程 压气机转子 数值模拟 模拟退火 响应面 power and mechanical engineering compressor rotor numerical simulation simulated annealing response surface
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参考文献6

  • 1Wadia A R,Szucs P N,Crall D W.Inner working of aerodynamic sweep[D].ASME Paper 97-GT-401. 被引量:1
  • 2June Chung,Ki D Lee.Shape optimization of transonic compressor blades using quasi-3D flowphysics[D].ASME Paper 2000-GT-489. 被引量:1
  • 3Ernesto Benini.Three-dimensional multi-objective design optimization of a transonic compressor rotor[J].Journal of Propulsion and Power,2004,20(3). 被引量:1
  • 4Dr Shahrokh Shahpar.A comparative study of optimisation methods for aerodynamic of turbomachienry blades[D].ASME Paper 2000-GT-523. 被引量:1
  • 5Chan-Sol Ahn,Kwang-Yong Kim.Aerodynamic design optimization of an axial flow compressor rotor[D].ASME Paper 2002-GT-30445. 被引量:1
  • 6Corana A,Marchesi M,Martini C,et al.Minimizing multimodal functions of continuous variables with the simulated annealing algorithm[J].ACM Transaction on Mathematical Software,1987,13(3),262-280. 被引量:1

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