• 제목/요약/키워드: HWA, 열선풍속계

검색결과 2건 처리시간 0.016초

Gun식 가스버너의 연소실내 난류 선회유동장 고찰 (Investigation on the Turbulent Swirling Flow Field within the Combustion Chamber of a Gun-Type Gas Burner)

  • 김장권
    • 대한기계학회논문집B
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    • 제33권9호
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    • pp.666-673
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    • 2009
  • The turbulent swirling flow field characteristics of a gun-type gas burner with a combustion chamber were investigated under the cold flow condition. The velocities and turbulent quantities were measured by hot-wire anemometer system with an X-type probe. The turbulent swirling flow field in the edge of a jet seems to cause a recirculation flow from downstream to upstream due to the unbalance of static pressure between a main jet flow and a chamber wall. Moreover, because the recirculation flow seems to expand the main jet flow to the radial and to shorten it to the axial, the turbulent swirling flow field with a chamber increases a radial momentum but decreases an axial as compared with the case without a chamber from the range of about X/R=1.5. As a result, these phenomena can be seen through all mean velocities, turbulent kinetic energy and turbulent shear stresses. All physical quantities obtained around the slits, however, show the similar magnitude and profiles as the case without a chamber within the range of about X/R=1.0.

덕트의 유무에 따른 Gun식 가스버너의 난류유동장 특성 고찰 (Investigation on the Turbulent Flow Field Characteristics of a Gun-Type Gas Burner with and without a Duct)

  • 김장권;정규조
    • 동력기계공학회지
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    • 제10권4호
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    • pp.17-24
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    • 2006
  • The turbulent flow field characteristics of a gun-type gas burner with and without a duct were investigated under the isothermal condition of non-combustion. Vectors and mean velocities were measured by hot-wire anemometer system with an X-type hot-wire probe in this paper. The turbulent flow field with a duct seems to cause a counter-clockwise recirculation flow from downstream to upstream due to the unbalance of static pressure between a main jet flow and a duct wall. Moreover, the recirculation flow seems to expand the main jet flow to the radial and to shorten it to the axial. Therefore, the turbulent flow field with a duct increases a radial momentum but decreases a axial momentum. As a result, an axial mean velocity component with a duct above the downstream range of about X/R=1.5 forms a smaller magnitude than that without a duct in the inner part of a burner, but it shows the opposite trend in the outer part.

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