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ANALYSIS OF TURBULENT BOUNDARY LAYER FLOWS USING A TIME MARCHING METHOD

시간 전진법을 이용한 난류 경계층 유동의 해석

  • Gong, H. (Dept. of Aerospace Engineering, Inha Univ.) ;
  • Lee, S. (Dept. of Aerospace Engineering, Inha Univ.)
  • 공효준 (인하대학교 항공우주공학과) ;
  • 이승수 (인하대학교 항공우주공학과)
  • Received : 2014.12.08
  • Accepted : 2015.01.13
  • Published : 2015.03.31

Abstract

A 3-dimensional compressible turbulent boundary layer solver has been developed. A time marching method is used to integrate the turbulent boundary layer equations. While the direct integration of the boundary layer equations is performed for unseparated flow regions, the inverse integration is performed for separated flow regions. The program is verified for flows that have analytical solutions or other numerical results. The solver will be merged with an Euler solver for viscous-inviscid interaction.

Keywords

References

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