• Proceedings of the Korea Water Resources Association Conference
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• 2005.05b
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• pp.351-356
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• 2005

출구부 수심을 결정하는 것은 개수로 흐름을 해석하는 데 매우 중요하면서도 쉽지 않은 일이다. 출구부 수심을 결정하기 위해서는 무엇보다도 정확한 관측이 선행되어야 한다. 그러나 종종 그 형상이 복잡하고 부정확한 관측결과를 가져오는 경우도 있다. 이 때문에 본연구진은 보다 더 효과적으로 마찰계수와 출구부 수심을 결정하는 방법을 제안하고자 한다. 출구부 수심은 그 흐름 특성에 따라 상류일 경우에는 임계수심, 사류일 경우에는 등류수심과 거의 일치하며 이를 통해 출구부 수심을 양해적으로 산정하는 방법을 제안한다. 이 양해식은 관측된 '정류수심'자료를 통해 개발 및 검증되었으며, 여기서 정류수심은 하수관의 출구부에서부터 대략 관경의 0.7배 정도 떨어진 지점을 중심으로 형성되는 수심을 가리킨다.

• Proceedings of the Korea Institute of Fire Science and Engineering Conference
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• 2010.04a
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• pp.255-260
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• 2010

최근 건축물은 초고층화 대형화 지하심층화 되어가고 있다. 한편, 이러한 건축물은 화재시 기존의 건축물 보다 피난안전성의 문제가 대두된다. 이에 따라 국내외에서는 성능적 피난안전계획을 목적으로 PBD를 시행하고 있다. 하지만 국내의 경우 국외에 비하여 그 방법론이 부족하고, 건축물의 피난용량이 부족한 시점에 놓여있다. 이러한 배경을 통하여 본 연구는 재실자 피난행동분석 중 피난계산에 중요한 요인인 출구유동계수를 조사하고, 기존의 국내외 문헌과 비교를 실시하였다. 이에 따라 종합표준치 1.88인/ms를 도출하였으며, 또한 실태조사의 한계성을 파악하고, 이를 통한 조사기법에 대한 프로세스를 제안하였다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.17 no.6
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• pp.650-655
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• 2016

In this study, a computational simulation of the internal flow characteristics was carried out for a Urea-SCR Injector. A single hole swirl injector with a swirl disk and slanted nozzle was used in this simulation. The maximum needle lift and opening velocity were selected as the design parameters. To analyze the unsteady internal flow characteristics of the Urea-SCR injector, the moving grid technique was applied to simulate the delicate needle movement. According to the simulation results, the injected mass flow rate from the Urea-SCR injector decreased with increasing needle opening velocity and maximum needle lift. This is because the Urea-solution tends to fill the empty space that the needle previously occupied. The swirl flow is decreased as the flow goes through the injector nozzle, because of the friction with the nozzle wall. Also, during the maximum needle lift period, the swirl coefficient and mean swirl coefficient increase with increasing needle lift. The results of this study may be used as the basic design data of related injectors.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.05a
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• pp.295-298
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• 2009

Bent ducts add loss and decrease efficiency. Many researchers have been conducted the performances of bent ducts, but their shapes of inlet and outlet are same. However, in this investigation, the focus is on a bent duct which is annular at the inlet and circular at the outlet. The bent duct of these complex shapes has not been investigated, but has been used in many fields. The performance of such bent duct is investigated under inlet speed 54 m/s and Re = 238,000. Wall static pressure tappings are located surface of the bent duct to measure the static pressure and a probe is traversed at the inlet and outlet of the bent duct to measure the total pressure. As a result, it presents static pressure distribution on the bent duct surface, streamwise velocity profile at inlet and outlet of the bent duct and total pressure loss profile at outlet. In this investigation, the total pressure loss coefficient is 0.243.

• Journal of the Korean Society of Propulsion Engineers
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• v.11 no.4
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• pp.19-25
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• 2007

A LNG safety valve functions to control a constant pressure inside the LNG line of transportation, and the flow through it accompanies with noise and vibration which affect adversely on the system. The present study aims at understanding the flow physics of LNG safety valve for a practical design of LNG safety valve. A computational work using the two-dimensional, axisymmetric, compressible, Navier-Stokes equations is carried out to simulate the gas flow through the LNG safety valve, and compared with the theoretical results. It is found that the shape of valve sheet and the gap size are the key parameters in determining the gas dynamic forces on the valve sheet, and there exists a distance between nozzle exit and valve sheet in which the thrust coefficient at the valve sheet increases abruptly.

• Proceedings of the Korea Water Resources Association Conference
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• 2006.05a
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• pp.510-514
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• 2006

하수관은 평상시 개수로 흐름특성을 가지며, 설계강우를 초과하는 홍수사상이 발생하는 경우에만 만수되어 관로 흐름특성이 나타난다. 개수로 흐름은 Froude수에 의해 상류와 사류로 구분되며, 일반적으로 등류수로로 가정한 후 유출량 또는 수심 등 흐름 변위를 산정한다. 사류인 경우 하수관 출구부에서 등류수심이 발생한다고 가정하면 해석이 용이하지만 길이가 짧은 하수관에서 실험을 수행한 결과 등류조건을 조성하기가 용이하지 않았다. 따라서 등류수심이 발생한다는 가정 하에 개발된 기존 마찰계수 산정식의 보완이 필요하다. 완변이 부등류 해석법을 이용하여 부등류 마찰계수 산정식을 개발하고자 시도하였으며, 이를 등류 마찰계수 산정식의 결과와 비교하였다.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.37 no.4
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• pp.377-385
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• 2013

To identify the effects of an outflow area on pool boiling heat transfer in a vertical annulus, three different flow restrictors were studied experimentally. For the test, a heated tube of smooth stainless steel and water at atmospheric pressure were used. Both annuli with open and closed bottoms were considered. To validate the effects of the outflow area on the heat transfer, the results of the annulus with the restrictor were compared with the data for the plain annulus without the restrictor. The reduction of the outflow area ultimately results in a decrease in the heat transfer. As the outflow area is very small, a slight increase in heat transfer is also observed. The major cause of this tendency is explained as the difference in the intensity of liquid agitation cause by the movement of coalesced bubbles. It is identified that the convective flow, pulsating flow, and evaporative mechanism are considered as the important mechanisms.

• Journal of the Korean Society of Propulsion Engineers
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• v.19 no.4
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• pp.1-7
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• 2015

A cavitation venturi is a device that allows a liquid flow rate to be fixed or locked independent of a downstream pressure and has been successfully used in a liquid rocket engine system which requires a stable propellant flow rate. In the present research, four cavitation venturis which have same dimensions except for converging inlet angle and diverging outlet angle, were designed and manufactured. Flow rates through each venturi and upstream/downstream pressures were measured by changing the pressures. From the experimental data, the discharge coefficients and critical pressure ratios were calculated for each venturi. It was found that the inlet and outlet angles of the cavitation venturi affected the discharge coefficient, and the outlet angle influenced on the critical pressure ratio.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.38 no.5
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• pp.431-436
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• 2014

Conductance is a concept contrary to flow resistance and is extensively used as a flow index on how easily fluid is transported through a pneumatic pipe or fluid device. However, research on flow conductance is very rare to date, and a systematic investigation is needed for the standardization of pneumatic devices. In the present study, a computational fluid dynamics method was applied to solve the compressible Navier-Stokes equations with two-equation turbulence models. The present CFD results were validated with existing experimental data. The conductance values and friction factors at the inlet and outlet of a pneumatic pipe were used to assess the flow rates. The present results showed that the conductance depends on the pressure ratio at the inlet and outlet of a pipe.

• Journal of the Korean Institute of Gas
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• v.21 no.3
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• pp.53-60
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• 2017

Various researches have been conducted for the reduction of NOx at the combustion furnace and exhaust gas recirculation method is commonly used technology for NOx reduction. The present research adopted coanda nozzles at the outside pipes of furnace to entrain the exhaust gas for the exhaust gas recirculation and the mixed gas was ejected to the tangential direction to cause the swirl flow in the furnace. The combustion flow characteristics in the exhaust gas recirculation burner with coanda nozzle has been elucidated by analyzing the swirl flow streamlines, temepraure and reaction rate distribution in the furnace. The exhaust gas entrained flow rate has been investigated by changing the excess air factor and coanda nozzle gap and the exhaust gas entrained flow rate increased with the increase of excess air factor and it decreased with the increase of coanda nozzle gap. The mean temperature at the exit plane of exhaust gas decreased with the excess air factor and it was little affected by the increase of coanda nozzle gap. The NOx mass fraction at the exhaust gas exit plane remarkably decreased with the excess air factor and it was also little affected by the increase of coanda nozzle gap.