• 한국연소학회지
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• 제6권2호
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• pp.15-22
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• 2001

A pressure-based, unstructured finite volume method has been applied to couple the chemical kinetics and fluid dynamics and to capture effectively and accurately the steep gradient flame field. The pressure-velocity coupling is handled by two methodologies including the pressure-correction algorithm and the projection scheme. A stiff, operator-split projection scheme for the detailed nonequilibrium chemistry has been employed to treat the stiff reaction source terms. The conservative form of the governing equations are integrated over a cell-centered control volume with collocated storage for all transport variables. Computations using detailed chemistry and variable transport properties were performed for two laminar reacting flows: a counterflow hydrogen-air diffusion flame and a lifted methane-air triple flame. Numerical results favorably agree with measurements in terms of the detailed flame structure.

• 한국자동차공학회논문집
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• 제4권5호
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• pp.130-141
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• 1996

Numerical study of a confined, swirling, isothermal and spray-combusting flows has been presented. The pressure-velocity coupling in the Eulerian gas-phase equation is handled by the improved PISO algorithm. The droplet dispersion by turbulence is introduced by a Stochastic Separated Flow(SSF) model. The k-$\varepsilon$ turbulence model and the eddy dissipation model are employed to account for turbulence-combustion interaction. The detailed comparison with experimental data has been made for the isothermal jet swirling flows and the nearly monodisperse spray-combusting flow in the swirl combustor.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2001년도 추계 학술대회논문집
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• pp.1-9
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• 2001

In this paper, some numerical methods recently developed for gas-liquid two-phase flows are reviewed. And then, a preconditioning method to solve cavitating flow by the author is introduced. This method employs a finite-difference Runge-Kutta method combined with MUSCL TVD scheme, and a homogeneous equilibrium cavitation model. So that it permits to treat simply the whole gas-liquid two-phase flow field including wave propagation, large density changes and incompressible flow characteristic at low Mach number. Finally, numerical results such as detailed observations of the unsteady cavity flows, a sheet cavitation break-off phenomena and some data related to performance characteristics of hydrofoils are shown.

• 대한원격탐사학회지
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• 제34권6_1호
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• pp.879-891
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• 2018

본 연구에서는 GIS 자료와 CFD 모델을 이용하여, 도시 재개발 및 건물 신축이 부경대학교 주변의 상세 흐름 변화에 미치는 영향을 조사하였다. 건설 전 후에 대한 부경대학교 내부와 주변 지역의 상세 흐름을 분석하기 위해, 건설 전 후의 16방위 유입류에 대하여 수치 모의 실험을 수행하였다. 장애물에 의한 마찰이 반영되지 않은 관측 풍속을 유입 경계 조건으로 사용하기 위해, 광안 등표기상관측장비에서 관측한 풍속 자료를 사용하였다. 건물 신축에 의한 부경대학교 내부의 대기 흐름 변화를 분석하기 위해, 건물 신축 이후에 16방위 유입류에 따라 풍속이 변화한 영역을 분석하였다. 동남동풍과 남풍이 부는 경우에 풍속 변화 영역이 넓게 나타났는데, 이는 수치 영역의 동쪽에 건설된 고층 건물과 부경대학교 남쪽에 건설된 아파트 단지와 공학관에 의한 영향이 크게 나타났기 때문이다. 대연 AWS(AWS 942)에서 최대 관측 빈도로 나타난 동풍이 부는 경우, 건설 후에 풍속이 변화한 영역은 비교적 좁게 나타났다. 수치 모의 결과를 통해 도시 재개발 및 건물 신축이 건설 지역의 풍하측 방향으로 멀리 떨어진 지역에도 영향을 미치는 것을 확인하였다. 또한, GIS 자료와 CFD 모델이 도시 재개발 및 건물 신축 계획 단계에서 건물 신축 이후의 상세 흐름을 분석하는데 유용함을 확인하였다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2005년도 추계 학술대회논문집
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• pp.81-85
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• 2005

Three-dimensional steady incompressible laminar entry flows in a square duct of $90^{\circ}$ bend are numerically simulated by a new solution code(PowerCFD) using unstructured cell-centered method. Solutions are obtained with three unstructured grid types of hexahedron, prism and hybrid at a Reynolds number, based on the hydraulic diameter and bulk velocity, of 790. Interesting features of the flow are presented in detail. Detailed comparisons between the computed solutions and the available experimental data are given mainly for the velocity distributions at cross-sections in a $90^{\circ}$ bend of a square duct with fully-developed entry flows. It is found that the code is capable of producing the nature of laminar flow in curved square duct with no grid type dependency.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2002년도 학술대회지
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• pp.683-686
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• 2002

The hydrodynamic instability of the three-dimensional boundary-layer over a rotating disk has been numerically investigated for three cases flows using linear stability theory (i.e. Rossby number, Ro = -1, 0, and 1). Detailed numerical values of the disturbance wave number, wave frequency, azimuth angle, radius (Reynolds number, Re) and other characteristics have been calculated for $K{\acute{a}}rm{\acute{a}}n$, Ekman and $B{\"{o}}ewadt$ boundary-layer flows. Neutral curves for these flows are presented. Presented are the neutral stability results concerning the two instability modes (Type I and Type II) by using a two-point boundary value problem code COLUEW that was based upon the adaptive orthogonal collocation method using B-spline. The prediction from the present results on both instability modes among the three cases agrees with the previously known numerical and experimental data well.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 1999년도 춘계 학술대회논문집
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• pp.66-72
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• 1999

A numerical simulation method has been under development for solving turbulent flows around a ship model in maneuvering motion using the Reynolds Averaged Navier-Stokes equations. The method used second-order finite differences, collocated grids, pressure-Poisson equation and four-stage Runge-Kutta scheme as key components of the solution method. A modified Baldwin-Lomax model is used for the turbulence closure. This paper presents a preliminary result of the computational study on turbulent flows past a ship model in drift motion. Calculations are carried out for a Series 60 $C_B=0.6$ ship model, for which detailed experimental data are available. The results of the present calculations are compared with the experimental data for hydrodynamic forces acting on the model as well as velocity distributions at longitudinal sections. Only fair agreements has been achieved. The computational results show the complex asymmetrical shear flow patterns including three-dimensional separations followed by formation of bilge vortices both in bow and stern regions.

• 천문학회지
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• 제34권4호
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• pp.281-283
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• 2001

As a companion to an adiabatic version developed by Ryu and his coworkers, we have built an isothermal magnetohydrodynamic code for astrophysical flows. It is suited for the dynamical simulations of flows where cooling timescale is much shorter than dynamical timescale, as well as for turbulence and dynamo simulations in which detailed energetics are unimportant. Since a simple isothermal equation of state substitutes the energy conservation equation, the numerical schemes for isothermal flows are simpler (no contact discontinuity) than those for adiabatic flows and the resulting code is faster. Tests for shock tubes and Alfven wave decay have shown that our isothermal code has not only a good shock capturing ability, but also numerical dissipation smaller than its adiabatic analogue. As a real astrophysical application of the code, we have simulated the nonlinear three-dimensional evolution of the Parker instability. A factor of two enhancement in vertical column density has been achieved at most, and the main structures formed are sheet-like and aligned with the mean field direction. We conclude that the Parker instability alone is not a viable formation mechanism of the giant molecular clouds.

• 동력기계공학회지
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• 제2권1호
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• pp.31-38
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• 1998

A diffuser, an important equipment to change kinetic energy into pressure energy, has been studied for a long time. Though experimental and theoretical researches have been done, the understanding of energy transfer and detailed mechanism of energy dissipation is unclear. As far as numerical prediction of diffuser flows are concerned, various numerical studies have also been done. On the contrary, many turbulence models have constraint to the applicability of diffuser-like complex flows, because of anisotropy of turbulence near the wall and of local nonequilibrium induced by an adverse pressure gradient. The existing $k-{\epsilon}$ turbulence models have some problems in the case of being applied to complex turbulent flows. The purpose of this paper is to test the applicability of the nonlinear $k-{\epsilon}$ model concerning diffuser-like flows with expansion and streamline curvature. The results show that the nonlinear $k-{\epsilon}$ turbulence model predicted well the coefficient of pressure, velocity profiles and turbulent kinetic energy distributions, however the shear stress prediction was failed.

• 대한원격탐사학회지
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• 제36권6_3호
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• pp.1643-1652
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• 2020

본 연구에서는 국지예보시스템(LDAPS)과 전산유체역학(CFD) 모델을 접합하여, 부산 중구 광복동에 소재한 건물 밀집 지역의 상세 흐름을 조사하였다. 도시 지역 기상에 대한 보다 현실적인 수치 모의를 위해 기상청이 현업으로 운용하는 LDAPS 결과로부터 기상 요소(풍향, 풍속, 온위)를 추출하여 CFD 모델의 초기·경계장으로 사용하였다. LDAPS로부터 추출한 기상 요소(U, V)는 공간 선형 보간법을 이용하여 CFD 모델의 수평·연직 격자에 맞게 내삽하였고, 공간 선형 보간법을 이용해 내삽한 온위는 CFD 모델의 각 격자점에서 온도로 변환된다. 본 연구에서는 건물 옥상에서 측정한 3차원 초음파 풍향·풍속계에서 측정한 풍속과 풍향을 이용하여 수치 모의 결과를 검증하였다. 대상 기간(2020년 6월 22일) 동안 측정 지점(PKNU-SONIC)에서는 바람이 약하게 나타났고, 새벽 시간에는 북동풍과 북서풍이 불었으며, 주간에는 주로 남동풍이 불었다. LDAPS-CFD 접합 모델은 측정 풍향과 풍속을 유사하게 수치 모의하였다. 07시에는 동북동쪽에서 유입되는 흐름이 지형과 건물에 의해 변화하였고, PKNU-SONIC 지점에서 수치 모의된 풍향(동남동풍)은 측정 풍향과 유사하다. 19시에는 남동쪽에서 유입되는 흐름이 PKNU-SONIC 지점까지 유입되어 측정 풍향과 유사하게 모의하였다.