Journal of computational fluids engineering (한국전산유체공학회지)

Korean Society of Computational Fluids Engineering (한국전산유체공학회)
권호 표지

A DESIGN OPTIMIZATION STUDY OF BLUNT NOSE HYPERSONIC FLIGHT VEHICLE MINIMIZING SURFACE HEAT-TRANSFER RATE AND DRAG

표면 열전달율과 항력을 최소화한 극초음속 비행체 선두부 형상 최적설계

  • 임설 (영남대학교 대학원 기계공학과) ;
  • 서정일 (국방과학연구소) ;
  • 김상덕 (영남대학교 기계공학부) ;
  • 송동주 (영남대학교 기계공학부)
  • Published : 2005.09.01
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Abstract

A design optimization of hypersonic flight vehicle has been studied by using upwind Navier-Stokes method and numerical optimization method. CFD method is linked to numerical optimization method by using a Bezier curve and a design optimization of blunt nose hypersonic flight vehicle has been studied. Heat transfer coefficient and drag coefficient are selected as objective functions or design constraints. The Bezier curve-based shape function was applied to blunt body shape.

Keywords