• Proceedings of the Korea Water Resources Association Conference
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• 2011.05a
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• pp.65-65
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• 2011

하천의 하구지역은 유역의 보전, 개발 논의가 매우 다양하게 전개되고 있는 지역으로 개발계획들로 인한 환경변화로 유출 특성 및 유사이동 변화에 따른 정밀한 조사연구를 통한 대처방안을 수립이 필요한 지역이다. 본 논문은 2차원 수치해석이 가능하고 복잡한 해안구조를 포함한 하구지역의 흐름해석이 가능한 MIKE21 FM 프로그램을 통하여 홍수기시의 조위조건변화에 따른 수치해석을 수행하여 자연하구역인 한강하구지역을 중심으로 수위 및 유사이동의 변화 특성을 분석하였다. 첨두유량 발생 시점과 하류경계조건의 변화에 따른 하구지역의 수위변화를 살펴보면, 대상 지역의 하천구간에 해당하는 전류수위표 지점에서 기수역 수로 지점에 비하여 변동폭이 가장 크게 나타났으며, 하류의 외해와 인접할수록 변동폭이 줄어드는 것으로 나타났다. 또한, 대상지역의 상류구간은 하천유량의 영향이 크기 때문에 상류구간일수록 창조시간에 비하여 낙조시간이 길게 분포되는 것으로 나타난다. 유사이동의 특성은 하천의 유속이 크게 감소하는 부분에 퇴적이 발생되며 강화북수로의 단면이 급격하게 변화하는 석모도와 교동도사이의 수로, 염하수로의 입구부분에서는 퇴적층이 발달하는 것으로 나타났다. 따라서, 한강하구와 같이 하구둑이 설치되지 않은 하천의 하구지역에 대해서는 상류와 하류 경계조건의 특성에 따라서 복잡한 수리학적 특성이 발생하기 때문에 개발이나 구조물 축조에 앞서 더욱 많은 현장조사와 특성분석을 통한 보다 정확한 경계조건의 구축이 필요할 것으로 사료된다.

• Clean Technology
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• v.29 no.4
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• pp.305-312
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• 2023

Due to the strengthening of environmental requirements, aging denitrification facilities need to improve their performance. The present study aims to suggest the possibility of improving performance using computational analysis techniques. This involved modifying both the geometric design and the operating conditions, including the flow path shape of the equipment such as the inlet guide vane and the curved diffusing part, and the flow control of the ammonia injection nozzle. The conditions presented in this study were compared with existing operating conditions in terms of the flow uniformity, the NH₃/NO molar ratio of the mixed gas flowing into the catalyst layer, and the total pressure drop of the facility. The flow field applied in the computational analysis ranged from the outlet of the economizer in the combustion furnace to the inlet of the air preheater, the full domain of the denitrification facility. The performances were derived by solving the flow fields using ANSYS-Fluent and the injection amount of ammonia was adjusted for each nozzle using Design Xplorer. Compared to the denitrification performances of the equipment currently in operation, the conditions proposed in this study showed an improvement in the flow uniformity and NH₃/NO composition ratio by 45.1% and 8.7%, respectively, but the total pressure drop increased by 1.24%.

• Journal of Advanced Marine Engineering and Technology
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• v.35 no.6
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• pp.809-813
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• 2011

Turbulent flows are numerically simulated in the three dimensional inlet duct for heat recovery steam generator. The present study is aimed to analyze the effect of a variation in turbulent flow pattern by the change of roof angle in the transition duct. The finite volume based Navier-Stokes equations with unstructured grids are solved to make clear the flow dynamic phenomena. Reviews are made on with the data of path lines, velocity vectors, dynamic pressure, residuals for numerical convergence and so on. The k-epsilon, k-omega, Reynolds stress and RNG k-epsilon are used for generation of turbulence. Two types of roof angle are applied with and without the swirl in the duct. Turbulent flow patterns could be investigated for the optimum duct design based on the computational results.

• Applied Chemistry for Engineering
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• v.26 no.1
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• pp.67-73
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• 2015

Using a computational fluid dynamics technique, the flow characteristics and particle residence time in a Taylor reactor were studied. Since flow characteristics in a Taylor reactor are dependent on the operating conditions, effects of the inlet flow velocity and reactor rotational speed were investigated. In addition, the particle residence time of $LiNiMnCoO_2$ (NMC), which is a cathode material in lithium-ion battery, is estimated in the Taylor vortex flow (TVF) region. Without considering the complex chemical reaction at the inlet, the effect of Taylor flow was studied. The results show that the particle residence time increases as the rotating speed increased and the flow rate decreased.

• Journal of Advanced Marine Engineering and Technology
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• v.37 no.1
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• pp.9-15
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• 2013

The effective use and management of energy resources has been issued to solve the global warming problem and petrolium price increase. To improve the energy efficiency of a heat exchanger, a new countermeasure is required and the heat transfer research of nano-fluids as a new working fluid is needed. This study was carried out with increasing the Reynolds number and the vol% of nano-fluids in the inlet temperature of $25^{\circ}C$ and $50^{\circ}C$. As the result, the higher the entrance temperature is, the higher the convective heat transfer coefficient is.

• Korean Journal of Bronchoesophagology
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• v.11 no.2 s.22
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• pp.10-15
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• 2005

식도와 인두 재건은 연하작용을 원활하게하고 발선기능을 보존하면서 위험부담이 가장 절은 술식을 선택하는 것이 원칙이다. 술식의 선택에 고려되어야 할 주요 인자는 결손부위의 크기, 창상의 상태, 술전 방사선치료 여부, 환자의 전신상태 등이다. 부분인두결손에는 유경근피판(pedicled myocutaneous flap)이나 유리피판이 적합하며 방사선 치료를 받은 경우는 유리피판이 유리하다. 흉곽입구 상부에 국한된 인두와 식도의 전체둘레결손에는 전완부, 외측 대퇴부, 공장의 유리피판이 좋다. 전완부는 피판이 다루기 쉽다는 장점이 있지만 공여부에 합병증이나 미용상의 문제가 있고 외측 대퇴부는 공여부의 문제는 매우 적으나 피판의 사용이 전완부에 비하여 약간 제한적이다. 공장은 허혈에 약하고 공여부 합병증이 다른 피판에 비해 불리하다. 저자의 경험으로는 흉곽상부에 국한된 결손의 재건에 환자가 비만하거나 대퇴부에 털이 많은 경우는 전완부 유리피판이 좋고 그렇지 않으면 외측 대퇴부 유리피판을 선택하는 것이 좋다고 생각된다. 흉곽입구 하방까지 연장된 결손이나 식도전적출술로 인한 결손에는 위전위술이 가장 적합하다. 방사선치료 등으로 창상에 혈관보호가 요구되는 경우는 대흉근피판이 유용하다. 앞으로 새로운 재건술의 개발이 이어지겠지만 모든 환자에게 맞는 이상적인 재건술은 없다. 재건술마다의 장단점과 제약점을 파악하고 환자의 조건에 따라 가장 적절한 재건술을 선택하는 것이 중요하다.

• Journal of the Korean Society of Propulsion Engineers
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• v.19 no.3
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• pp.65-72
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• 2015

In present study, a supersonic inlet for dual mode ramjets or RBCC/TBCC engines with a wide range of flight Mach numbers is designed. A conical variable inlet configuration is chosen for the inlet design. Geometric relations with angles of compression cones and conical shock waves are used for the design of the inlet configuration. The performance of the supersonic inlet is confirmed by the numerical analysis. The capture area ratio is maintained around 100% from Mach 3 to 8 conditions.

• Journal of the Korean Society of Propulsion Engineers
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• v.13 no.2
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• pp.54-63
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• 2009

Large eddy simulation was conducted for flow development in a chamber with wall injection which simulates the cold flow in an idealized hybrid rocket motor. It was found that a peculiar timescale, roughly corresponding to St~0.5, resides in the flowfield resulting from the interaction between the main oxidizer and wall injected flows. However, the fact that this time characteristics is absent in the temperature field in the vicinity of the wall indicates that even a small regression rate renders the passive scalar, such as temperature, dissimilar to the velocity field. This implies that a classical approach, which assumes that constant turbulent Prandtl number, should be replaced by a more sophisticated turbulence models to accurately predict the temperature field in the hybrid motor.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.6
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• pp.72-78
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• 2003

In the present paper, computational studies on the hydrodynamic behavior of the inducer for the rocket-engine turbopump are presented including the effect of the mass flow rate. As the mass flow rate is increased, the inducer showed better performance with weak back flows which may have deleterious effects upon the anti-cavitation ability. But the adopted inducer showed low head rise with high volume flow rates, which may be caused by the small passage area near the trailing edge. The static pressure distributions at the shroud surface are compared with experimental results showing very good agreements except near the leading edge where strong back flows are present. The overall performance of the inducer such as, efficiency, head rise is also compared with experiments. The computational results are generally in good agreements with experimental ones near the design point, but two results show discrepancy at the high flow rate.

• Plant Journal
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• v.9 no.2
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• pp.42-45
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• 2013

The worldwide issue of greenhouse gas reduction has recently drawn great attention to carbon capture and storage(CCS). In this study, we developed a 10,000 ton/year pilot injection plant for geological storage of carbon dioxide. Major components of the pilot plant include a pressure pump, a booster pump, and an inline heater to bring liquid carbon dioxide into its supercritical state. The test results show that the pilot plant readily achieves the injection pressure and temperature, showing satisfactory control performance. The overall power consumption is 2,000 ~ 2,500 W, more than 75% of which consumed by the pressure pump. This study will facilitate varied research on greenhouse gas reduction as the only domestically developed system for geological injection.