• Proceedings of the KAIS Fall Conference
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• 2010.05b
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• pp.1133-1136
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• 2010

2600cc급 디젤엔진의 냉각수 유동특성 개선을 위한 수치해석적 방법을 제시하기 위하여 본 연구가 수행되었다. 실린더 블록 및 헤드의 유동특성 분석을 위하여 개스킷 냉각수 통로의 면적과 갯수가 중점적으로 고려되었다. 베이스 모델의 수치해석적 분석에서 입구측에 치우친 냉각수 홀의 배치에 의하여 1, 2번 실린더 헤드로만 주 유동이 발생되었다. 이러한 문제점을 개선하기 위하여 개스킷 냉각수 통로를 재설계하였다. 수정모델은 주 유동이 4번 실린더 측으로 유도되었으며, 배기밸브 사이의 유동도 개선되었다. 재설계과정에서 개스킷 냉각수통로의 전체면적을 고려치 않게 되면 유량이 줄어들게 되는 문제점이 발견되었다. 본 연구를 통하여 실린더 헤드와 블록사이의 냉각수 유동을 제어하는 개스킷의 중요성을 확인하였으며, 냉각수 유동특성 최적화는 개스킷 홀의 총 면적을 고려하여 냉각수의 총질량유량을 설계하여야 한다.

• Proceedings of the KAIS Fall Conference
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• 2012.05b
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• pp.665-667
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• 2012

본 논문에서는 시작엔진 제작에 앞서 CFD기법을 이용하여 디젤 엔진의 블록과 헤드에서의 냉각수 유동 특성을 분석하고자 하였다. 유동 해석 결과 1번 실린더를 거쳐 4번 실린더까지 유동이 원활하게 흐르는 것을 확인 할 수 있었다. 이는 전체적인 냉각수 분배에 영향을 미쳐 엔진 설계 시 발생할 수 있는 3, 4번 실린더의 과열을 방지 할 수 있을 것으로 판단된다. 또한, 열전달 계수가 전체적으로 균일하게 분포되어 냉각수의 열전달 특성이 양호할 것으로 판단된다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.10 no.12
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• pp.3553-3558
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• 2009

This study has been conducted to improve coolant flow pattern in the gasoline engine. Flow field has been calculated for the coolant passage mainly around the exhaust ports and valves. For the original model, a flow stagnant region has existed between exhaust valves of the second cylinder. To improve coolant flow characteristics, coolant passage area has been re-modeled and optimized. Furthermore, for the improved coolant core model, coolant passage under the exhaust manifold has been added to reduce exhaust-gas temperature. It was found that the flow through a gasket plays a critical role for the flow in the cylinder head and around exhaust valves. Finally, coolant flow around exhaust valves and in the cylinder head has been improved in terms of flow rate distribution.

• Aerospace Engineering and Technology
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• v.12 no.1
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• pp.163-172
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• 2013

In this study, the cooling of rocket exhaust plume by sprayed water inside plume were investigated as varying of sprayed water mass, location, and method using computational fluid analysis. For Analyze rocket exhaust plume, a single species unreacted analysis model based on the chemically frozen analysis was used and the discrete particle model which was a kind of Euler-Lagrangian analysis model was used for simulate sprayed water inside plume. It was confirmed that the temperature of plume was reduced without cooling when water mass was two times of plume mass through analysis results.

• Proceedings of the KIPE Conference
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• 2014.11a
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• pp.161-162
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• 2014

본 연구의 목적은 HVDC Valve module 및 valve tower에 유입되는 냉각 유체의 유동장 동적 해석과 동시에 냉각 유체의 동적 특성을 측정 비교함으로써 유동 해석의 적합성을 판단하고, HVDC valve module과 valve tower의 냉각 유로 및 관련 기구 설계의 기초 자료로 활용하는데 그 목적이 있다.

• Proceedings of the Korean Nuclear Society Conference
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• 2002.10a
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• pp.189.2-189
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• 2002

• Proceedings of the KSME Conference
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• 2005.11a
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• pp.34.2-34.2
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• 2005

• Journal of the Korean Institute of Gas
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• v.16 no.2
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• pp.9-13
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• 2012

The present study has been carried out to diagnose the temperature safety of a boiler desuperheater which decreases abnormally higher temperature of superheated steam in a reheater of a power plant. The liquid water in the desuperheater stays in a closed space. It becomes heated by the high temperature superheated steam and boiling could occur. Boiling might increase internal pressure and it could destroy the desuperheater if the internal pressure exceeds the allowable pressure of the desuperheater. The present study modeled reasonably the desuperheater and four cases of heat transfer analysis are executed with the consideration of insulator and natural convective fluid flow of the inside cooling water. For the case excluded the natural convective fluid flow, the temperature exceeds the allowable temperature and pressure. On the other hand, for the real case included natural convective fluid flow and insulator, the active heat transfer from higher temperature region to lower temperature region occurs and it makes the temperature in the cooling water below the allowable temperature and pressure. From this fact, it could be thought that the desuperheater in the reheater is safe from destroy or back flow.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.112-115
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• 2017

We analyzed the rocket engine flow to check whether the possibility of the ground test and the equipment safety problems in the high altitude engine test facility. The test condition is that the vacuum chamber is open and the coolant water is injected into the supersonic diffuser. The analysis uses two-dimensional axisymmetry with a mixture of plume, air, and cooling water. As a result, the ground test was possible up to the cooling water flow rate of 200 kg/sec. However, due to the back flow of the initial plume, the vacuum chamber is exposed to high temperature, and at the same time, the inside of the vacuum chamber is contaminated due to the reverse flow of the cooling water. Therefore, sufficient insulation measures and work for pollution avoidance should be preceded.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.1021-1025
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• 2017

Numerical heat/flow analysis was performed on a liquid rocket engine head with the cooling water manifold to ensure the durability of a ground test facility for heat exchanger. Through these studies, the shapes of the injector and the flow path were determined and applied to the head of the engine under development. Firing tests were conducted to verify the designed coolant manifold and no thermal damage was found on the engine-head-face. Comparing the combustion test results with the numerical analysis, the outlet temperature of coolant showed a difference of about $15^{\circ}C$. This trend is reasonable considering existence of LOX manifold, thermal barrier coating, and the actual location of flame.