A Study on 2-D Airfoil Design Optimization by Kriging

Kriging 방법을 이용한 2차원 날개 형상 최적설계에 대한 연구

  • 가재도 (한국과학기술원 항공우주공학과) ;
  • 권장혁 (한국과학기술원 항공우주공학과)
  • Published : 2004.03.01

Abstract

Recently with growth in the capability of super computers and Parallel computers, shape design optimization is becoming easible for real problems. Also, Computational Fluid Dynamics(CFD) techniques have been improved for higher reliability and higher accuracy. In the shape design optimization, analysis solvers and optimization schemes are essential. In this work, the Roe's 2nd-order Upwind TVD scheme and DADI time march with multigrid were used for the flow solution with the Euler equation and FDM(Finite Differenciation Method), GA(Genetic Algorithm) and Kriging were used for the design optimization. Kriging were applied to 2-D airfoil design optimization and compared with FDM and GA's results. When Kriging is applied to the nonlinear problems, satisfactory results were obtained. From the result design optimization by Kriging method appeared as good as other methods.

Keywords

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