• 대한기계학회논문집B
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• 제38권12호
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• pp.991-997
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• 2014

이 연구는 Gun식 가스버너의 스월유동장을 연소실과 화염이 없는 상태에서 직선형 5공압력프로브의 측정을 통해 고찰하였다. 직선형 5공압력프로브에 의한 속도 및 정압성분들은 넌널링 교정방법에 의해 연산하였으며, X형 열선프로브와 전산유체역학의 해석에 의한 결과들과 비교하였다. 결과적으로 Gun식 가스버너의 중심부에서 스월유동장에 대해 5공압력프로브에 의한 속도 및 정압의 측정값들은 비교적 X형 열선프로브에 의한 경우보다는 좋은 성능을 보였으나 전산유체역학의 해석에 의한 경우보다는 다소 미흡한 결과를 보였다.

• 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.

• 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.