• 한국도로학회논문집
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• 제7권2호
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• pp.57-67
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• 2005

거의 대부분의 문헌에서 아스팔트바인더의 유동거동을 다룰 때, 단일상 균일 유체로 일률적으로 취급하는데 이로 인한 오류가 심각하다. 본 연구에서는 개질이던 스트레이트이던 아스팔트바인더의 유동과 관련된 특성방정식을 모두 소개하고, 특히 다상 불균일 유체의 특성방정식을 새로이 소개한다. 이러한 식들의 특징 이 무엇인지를 실제 측정된 아스팔트바인더의 동전단시험 데이터를 이용하여 설명한다 특히 단일상 균일 유체와 다상 불균일 유체와의 거동차이전과 특성방정식의 차이점에 대해 집중 부각한다. 이러한 차이는 아스팔트유체를 다룰 때 어떠한 특성방정식을 사용해야 하며,특정 바인더를 분석하기 위해서는 어떤 물성을 조사해야 하는 지에 대해서 이해하게 한다. 본 연구는 개질바인더의 분석과 등급제정에 필수적인 정보를 제공한다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2005년도 추계 학술대회논문집
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• pp.169-177
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• 2005

A high resolution scheme for solving gas-liquid two-phase flows with cavitation is described. This scheme uses the curvilinear coordinate grid and solves the density based momentum equations for mixture of gas-liquid medium with a preconditioning method to treat both compressible and incompressible flow characteristics. The present preconditioned method is based on the Runge-Kutta explicit finite-difference scheme, and is improved by using the diagonalization, the flux difference splitting and the MUSCL-TVD schemes to save computational effort and to increase stability and resolvability, especially at gas-liquid contact surfaces. A homogeneous equilibrium cavitation model is used to treat the gas-liquid two-phase medium in cavitating flow as a locally homogeneous pseudo-single-phase medium. Therefore, it is easy to solve cavitating flow, including wave propagation, large density changes and incompressible flow characteristic at low Mach number. Some numerical results obtained by the present scheme are shown.

• Nuclear Engineering and Technology
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• 제40권2호
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• pp.133-138
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• 2008

The use of Supercritical Fluids(SCF) has been proposed for numerous power cycle designs as part of the Generation IV advanced reactor designs, and can provide for higher thermal efficiency. One particular area of interest involves the behavior of SCF during a blowdown or depressurization process. Currently, no data are available in the open literature at supercritical conditions to characterize this phenomenon. A preliminary computational analysis, using a homogeneous equilibrium model when a second phase appears in the process, has shown the complexity of behavior that can occur. Depending on the initial thermodynamic state of the SCF, critical flow phenomena can be characterized in three different ways; the flow can remain in single phase(high temperature), a second phase can appear through vaporization(high pressure low temperature) or condensation(high pressure, intermediate temperature). An experimental facility has been built at the University of Wisconsin to study SCF depressurization through several diameter breaks. The preliminary results obtained show that the experimental data can be predicted with good agreement by the model for all the different initial conditions.

• 한국세라믹학회지
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• 제48권3호
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• pp.236-240
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• 2011

In order to deposit a homogeneous and uniform ${\beta}$-SiC films by chemical vapor deposition, we demonstrated the phase stability of ${\beta}$-SiC over graphite and silicon via computational thermodynamic calculation considering pressure, temperature and gas composition as variables. The ${\beta}$-SiC predominant region over other solid phases like carbon and silicon was changed gradually and consistently with temperature and pressure. Practically these maps provide necessary conditions for homogeneous ${\beta}$-SiC deposition of single phase. With the thermodynamic analyses, the CVD apparatus for uniform coating was modeled and simulated with computational fluid dynamics to obtain temperature and flow distribution in the CVD chamber. It gave an inspiration for the uniform temperature distribution and low local flow velocity over the deposition chamber. These calculation and model simulation could provide milestones for improving the thickness uniformity and phase homogeneity.

• 소음진동
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• 제6권2호
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• pp.163-177
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• 1996

An investigation on thermohydraulic stability of flow oscillations in the CANada Deuterium Uranium-600(CANDU-6) heat transport system has been conducted. Flow oscillations in reactor coolant loops, comprising two heat sources and two heat sinks in series, are possibly caused by the response of the pressure to extraction of fluid in two-phase region. This response consists of two contributions, one arising from mass and another from enthalpy change in the two-phase region. The system computer code used in the investigation os SOPHT, which is capable of simulating steady states as well as transients with varying boundary conditions. The model was derived by linearizing and solving one-dimensional, homogeneous single- and two-phase flow conservation equations. The mass, energy and momentum equations with boundary conditions are set up throughout the system in matrix form based on a node-link structure. Loop stability was studied under full power conditions with interconnecting the two compressible two phase regions in the figure-of-eight circuit. The dominant function of the interconnecting pipe is the transfer of mass between the two-phase regions. Parametric survey of loop stability characteristics, i. e., damping ratio and period, has been made as a function of geometrical parameters of the interconnection line such as diameter, length, height and orifice flow coefficient. The stability characteristics with interconnection line has been clarified to provide a simple criterion to be used as a guide in scaling of the pipe.

• Korean Chemical Engineering Research
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• 제57권5호
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• pp.628-636
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• 2019

다양한 산업 공정에서 배관은 각 단위공정 사이의 연결 매개체의 역할을 하며, 내부의 유동에 있어 필수적인 장치이다. 따라서 배관의 최적설계는 안전과 비용의 측면에서 매우 중요한 문제이며, 설계 시 필수적인 사항은 배관 내 압력강하 및 유속, 배관 지름 등을 결정하는 일이다. 본 연구에서는 배관 지름 및 유속이 정해졌을 때 발생하는 압력강하, 배관의 압력강하 및 유속이 정해졌을 때의 배관 지름, 배관 지름 및 압력강하가 정해졌을 때의 유속을 결정하는 소프트웨어를 개발하였다. 배관 내 유동을 단일 상 흐름, 균질 2 상 유동, 분리 2 상 유동으로 구분하였으며 이에 따라 적절한 계산 모델을 적용하였다. 파이프의 재질 및 상대 거칠기, 유체의 물성치, 마찰계수의 계산을 위한 시스템 라이브러리를 구축하여 사용자의 입력을 최소화하였다. 배관 재질에 따른 가격 라이브러리를 구축하여 단위 길이당 배관 투자 비용의 산출을 가능하도록 구성하였다. 이러한 모든 기능은 사용자 편의를 위한 그래픽 사용자 인터페이스를 이용한 통합 환경에서 구현할 수 있으며, C# 언어를 개발 언어로 사용하였다. 소프트웨어의 정확도를 문헌 자료와 실 수행 과제의 예제를 통하여 검증하였으며 단일 상의 경우 1% 미만, 2 상의 경우 최고 8.8% 정도의 차이를 보였으며, 이에 따라 개발된 소프트웨어가 실제 공정의 계산에 유용하게 쓰일 수 있음을 알 수 있었다.

• 한국수소및신에너지학회논문집
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• 제33권6호
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• pp.808-818
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• 2022

In this research paper, we investigated the cryogenic line chill down characteristics of liquefied natural gas (LNG). A numerical analysis model was established and verified so that it can calculate the precise cooling characteristics of cryogenic fluid for the stable and safe utilization especially such as LNG and liquid hydrogen. The numerical modeling was programmed by C++ as an one-dimensional homogeneous model. The thermohydraulic cooling process was simulated using mass, momentum, energy conservation equations and appropriate heat transfer correlations. In this process, the relevant heat transfer correlations for nuclear boiling, transition boiling, film boiling, and single-phase heat transfer that can predict the experimental results were implemented. To verify the numerical modeling, several cryogenic line chill down experiments using LNG were conducted at the Korea Institute of Machinery & Materials (KIMM) LNG and Cryogenic Technology Center.

• Advances in aircraft and spacecraft science
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• 제9권5호
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• pp.415-431
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• 2022

Secondary flows have a huge impact on losses generation in modern low pressure gas turbines (LPTs). At design point, the interaction of the blade profile with the end-wall boundary layer is responsible for up to 40% of total losses. Therefore, predicting accurately the end-wall flow field in a LPT is extremely important in the industrial design phase. Since the inlet boundary layer profile is one of the factors which most affects the evolution of secondary flows, the first main objective of the present work is to investigate the impact of two different inlet conditions on the end-wall flow field of the T106A, a well known LPT cascade. The first condition, labeled in the paper as C1, is represented by uniform conditions at the inlet plane and the second, C2, by a flow characterized by a defined inlet boundary layer profile. The code used for the simulations is based on the Discontinuous Galerkin (DG) formulation and solves the Reynolds-averaged Navier-Stokes (RANS) equations coupled with the Spalart Allmaras turbulence model. Secondly, this work aims at estimating the influence of viscosity and turbulence on the T106A end-wall flow field. In order to do so, RANS results are compared with those obtained from an inviscid simulation with a prescribed inlet total pressure profile, which mimics a boundary layer. A comparison between C1 and C2 results highlights an influence of secondary flows on the flow field up to a significant distance from the end-wall. In particular, the C2 end-wall flow field appears to be characterized by greater over turning and under turning angles and higher total pressure losses. Furthermore, the C2 simulated flow field shows good agreement with experimental and numerical data available in literature. The C2 and inviscid Euler computed flow fields, although globally comparable, present evident differences. The cascade passage simulated with inviscid flow is mainly dominated by a single large and homogeneous vortex structure, less stretched in the spanwise direction and closer to the end-wall than vortical structures computed by compressible flow simulation. It is reasonable, then, asserting that for the chosen test case a great part of the secondary flows details is strongly dependent on viscous phenomena and turbulence.