A Computational Model on Shock-Vortex Interaction and Acoustic Radiation

충격파-와동 간섭 및 음향 방사에 대한 수치 모델

  • 장세명 (서울대학교 기계/항공공학부 공력소음 및 소음제어 연구실) ;
  • 이수갑 (서울대학교 기계/항공공학부) ;
  • 장근식 (한국과학기술원(KAIST) 기계공학과 항공우주공학)
  • Published : 2000.05.01

Abstract

We study a conceptual numerical model on shock-vortex interaction setting an impulsive shock in a compressible vertex. Navier-Stokes equations are solved for the investigation of interactive structure and acoustic wave propagation. The rotationally symmetric vortex enforces two compression-expansion pairs resultantly forming a quadrupolar shape. These compressive and expansive waves cylindrically propagate to the far field and turn to acoustic waves. Using a fine uniform Cartesian grid system and a TVD-high resolution method, the flow data irl: precisely obtained to extend our interest to the sound source.

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