한국전산유체공학회:학술대회논문집

Korean Society of Computational Fluids Engineering (한국전산유체공학회)
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Application of the Automatic Differentiation to Aerodynamic Design Optimization

자동미분의 공력최적설계 적용

  • 이재훈 (한국과학기술원 항공우주전공) ;
  • 김수환 (한국과학기술원 항공우주전공) ;
  • 안중기 (한국과학기술원 항공우주전공) ;
  • 권장혁 (한국과학기술원 항공우주전공)
  • Published : 2004.10.01
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Abstract

In gradient based optimization methods, the finite differencing which uses small perturbations in the design variables has been used to calculate the sensitivity. Recently, the automatic differentiation has been widely studied to calculate the function value and the sensitivities simultaneously. In this paper, the applicability of the automatic differentiation In the aerodynamic design optimization is studied. ADIFOR and TAPENADE are used to generate the codes which give the function value and the sensitivities for 2D compressible inviscid flows.

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