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Aerodynamic airfoil design using the Euler equations based on the dynamic evolution method and the control theory 被引量:5

Aerodynamic airfoil design using the Euler equations based on the dynamic evolution method and the control theory
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摘要 Based on the idea of adjoint method and the dynamic evolution method,a new optimum aerodynamic design technique is presented in this paper.It can be applied to the optimum problems with a large number of design variables and is time saving.The key of the new method lies in that the optimization process is regarded as an unsteady evolution,i.e.,the optimization is executed,simultaneously with solving the unsteady flow governing equations and adjoint equations.Numerical examples for both the inverse problem and drag minimization using Euler equations have been presented,and the results show that the method presented in this paper is more efficient than the optimum methods based on the steady flow solution and the steady solution of adjoint equations. Based on the idea of adjoint method and the dynamic evolution method, a new optimum aerodynamic design technique is pre- sented in this paper. It can be applied to the optimum problems with a large number of design variables and is time saving. The key of the new method lies in that the optimization process is regarded as an unsteady evolution, i.e., the optimization is exe- cuted, simultaneously with solving the unsteady flow governing equations and adjoint equations. Numerical examples for both the inverse problem and drag minimization using Euler equations have been presented, and the results show that the method presented in this paper is more efficient than the optimum methods based on the steady flow solution and the steady solution of adjoint equations.
机构地区 School of Aerospace
出处 《Science China(Physics,Mechanics & Astronomy)》 SCIE EI CAS 2011年第4期697-702,共6页 中国科学:物理学、力学、天文学(英文版)
关键词 演化方法 欧拉方程 控制理论 气动设计 空气动力学设计 基础 翼型 伴随方程 Euler equations, aerodynamic optimization, dynamic evolution, adjoint method
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参考文献7

  • 1A. Jameson,L. Martinelli,N.A. Pierce.Optimum Aerodynamic Design Using the Navier–Stokes Equations[J].Theoretical and Computational Fluid Dynamics (-).1998(1-4)
  • 2Antony Jameson.Aerodynamic design via control theory[J].Journal of Scientific Computing.1988(3)
  • 3Bauer F,Garabedian P,Korn D.A theory of supercritical wing sec-tions with computer programs and examples[].Lecture Notes in Economical and Mathematical Systems.1972
  • 4Zhang H X,Shen M Y.The optimization method based on dynamic evolution[].Proceedings of Modern Aerodynamic Seminar.2005
  • 5A Jameson,J Reuther.Control Theory Based Airfoil Design Using the Euler Equations. AIAA Paper 94-4272 . 1994
  • 6Alessandro Vivini,Domenico Quagliarella Z.Inverse and direct airfoil design using a multiobjective genetic algorithm[].AIAA Journal.1997
  • 7Lighthill M J.A new method of two-dimensional aerodynamic design[]..1945

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