• Title/Summary/Keyword: 개방된 충격파관

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NUMERICAL ANALYSIS FOR A SILENCER OF TANK GUN (대구경 화포의 소음기에 대한 수치해석)

  • Ko S. H.;Lee D. S.;Woo S. D.;Kang K. J.
    • Journal of computational fluids engineering
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    • v.10 no.4 s.31
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    • pp.59-65
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    • 2005
  • A numerical analysis was made to investigate the simple silencer for high pressure blast flow fields. Reynolds-Averaged Navier-Stokes equations were solved for an axisymmetric computational domain constructed by multi block grids. A blast flow field without the silencer was also calculated to validate the present numerical method. The effect of pressure diminution for the silencer was calculated by comparing with and without silencer at the atmosphere region. It was found that the tested silencer could achieve 89.4 percent pressure diminution.

Numerical Analysis for a Simple Shape Silencer for Intensity Diminution of High Pressure Blast Flow Fields (고압 폭발 유동장의 강도 감소를 위한 간단한 형상의 소음기에 대한 수치해석)

  • Ko S. H.;Woo S. D.;Kang K. J.
    • 한국전산유체공학회:학술대회논문집
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    • 2004.10a
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    • pp.91-94
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    • 2004
  • A numerical analysis was made to investigate the intensity diminution of a simple silencer for high pressure blast flow fields. Reynolds-Averaged Wavier-Stokes equations were solved for an axisymmetric computational domain constructed by multi block Chimera grids. A blast flow field without the silencer was also calculated to validate the present numerical method. The evolution of high pressure blast flow fields was observed by depicting calculated contours of pressure and Mach number. It was found that the tested silencer could achieve 76 percent intensity diminution.

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