THE STUDY OF AERO-ACOUSTICS CHARACTERISTIC BY BOUNDARY CONDITIONS

경계조건에 따른 공력음향 특성에 관한 연구

  • 이상수 (한국항공우주산업(주)) ;
  • 김재수 (조선대학교 항공우주공학과)
  • Published : 2009.04.24

Abstract

The present paper focuses on the analysis of aero-acoustics characteristic by several boundary conditions. In this simulation, a high-order and high-resolution numerical schemes are used for the accurate computation of compressible flow with several boundary conditions including characteristic boundary conditions as well as extrapolation and zonal characteristic boundary condition. These boundary conditions are applied to the computation of two dimensional circular cylinder flows with Mach number of 0.3 and Reynolds number of 400. The computation results are validated with measurement datum and other computation results for the Strouhal frequency of vortex shedding, the mean drag coefficient and root-mean-square lift for the unsteady periodic flow regime. Secondary frequency is predicted by three kinds of boundary conditions characteristic.

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