DEVELOPMENT OF A 2-D UNSTEADY FLOW SIMULATION CODE USING CARTESIAN MESHES

직교격자를 이용한 2차원 비정상 유동해석 코드 개발

  • 정민규 (한국과학기술원 항공우주공학과) ;
  • 이재은 (한국과학기술원 항공우주공학과) ;
  • 박세연 (한국과학기술원 항공우주공학과) ;
  • 권오준 (한국과학기술원 항공우주공학과) ;
  • 권장혁 (한국과학기술원 항공우주공학과) ;
  • 신하용 (한국과학기술원 산업공학과)
  • Published : 2009.04.24

Abstract

A two-dimensional unsteady inviscid flow solver has been developed for the simulation of complex geometric configurations on adaptive Cartesian meshes. Embedded condition was used for boundary condition and a predictor-corrector explicit time marching scheme was used for time-accurate numerical simulation. The Cartesian mesh generator, which was previously developed for steady problem, was used grid generation for unsteady flow. The solver was based on ALE formulation for body motion. For diminishing the effects of cut-cells, the cell merging method was used. Using cell merging method, it was eliminated the CFL constraints. The conservation problem, which is caused cell-type variation around region swept by solid boundary, was also solved using cell merging method. The results are presented for 2D circular cylinder and missile launching problem.

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