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TWO-DIMENSIONAL COMPUTATIONAL AEROACOUSTICS SIMULATION OF SOUND GENERATED BY FLOW AROUND A CIRCULAR CYLINDER

CAA를 이용한 2D 원형 실린더 공력 소음 해석

  • Park, I.C. (Dept. of Aerospace Engineering, Graduate School, Chungnam Nat'l Univ.) ;
  • Go, Y.J. (Dept. of Aerospace Engineering, Graduate School, Chungnam Nat'l Univ.) ;
  • Choi, J.S. (Dept. of Aerospace Engineering, Chungnam Nat'l Univ.) ;
  • Kim, B.S. (Dept. of Aerospace Engineering, Chungnam Nat'l Univ.)
  • 박인철 (충남대학교 대학원 항공우주공학과) ;
  • 고영주 (충남대학교 대학원 항공우주공학과) ;
  • 최종수 (충남대학교 항공우주공학과) ;
  • 김병수 (충남대학교 항공우주공학과)
  • Received : 2012.02.11
  • Accepted : 2013.03.16
  • Published : 2013.03.31

Abstract

Researches in the area of aeroacoustics have been conducted by two methods. In the first method theoretical formula or experimentation are utilized, and in the second method flow field analysis and acoustic analogy are utilized. In contrast to the first method, the second method does not need new experiments for every individual change of flow configurations and conditions, and it can predict their effects by the flow field analysis, which makes the second method preferred than the first one. In this paper numerical analysis to predict noise generated by a turbulent flow about a two dimensional circular cylinder by use of CAA (Computational Aeroacoustics) method is conducted and the results are compared to the available experimental data.

Keywords

References

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