• 한국항공우주학회지
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• 제40권8호
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• pp.647-654
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• 2012

외부 환경조건에 의한 항공기 위협인자로서 과냉각 대형 액적은 그 중요성이 지속적으로 보고되고 있다. 이러한 대형 액적의 거동은 상대적으로 작은 액적과 달리 그 형태가 변화하며 액적이 표면과 충돌시 파편이 발생하는 등 다양한 물리적 특성을 나타낸다. 이러한 대형 액적의 거동을 시뮬레이션 하기 위해 비정렬 격자계 기반 2차원 압축성 Navier-Stokes 코드와 액적 거동 시뮬레이션 코드를 개발하였다. 또한 대형 액적의 물리적 현상을 모사하기 위해 반경험적 기법에 기반한 액적항력모델과 액적-고체표면 충돌 모델을 기존 액적장 지배방정식의 액적항력계수 및 경계면의 수치적 경계조건으로 적용하였다. 그 결과 풍동 시험과 액적충돌 영역 및 최대 축적율은 매우 유사하게 나타난 반면 NACA23012 익형의 아랫면 주위 축적율의 경향은 풍동 시험보다 다소 크게 나타났다.

• 한국해양환경ㆍ에너지학회지
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• 제10권4호
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• pp.218-226
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• 2007

본 연구는 생존성 측면에서 잠수함의 내충격 설계시 고려해야 하는 수중폭발 충격응답해석 기법에 관하여 고찰하였다. 생존성을 고려하는 것은 현대의 모든 함정설계에 필수요건이며, 특히 잠수함의 수중폭발에 대한 내충격 설계는 반드시 고려되어야 할 사항이다. 기존의 수중함에 대한 내충격 설계는 가정된 이론에 의한 충격가속도를 정적해석의 결과를 통하여 단순하게 적용하였으나 본 연구에서는 직접해석법에 수중폭발 충격응답해석을 수행함으로써 기존의 방법보다 매우 합리적이고 신뢰성 높은 결과를 제시하였다. 특히 본 연구에서는 직접해석법 중에서 기존 수상함에서 널리 사용하고 있는 LS-DYNA/USA code일 적용보다 LS-DYNA code만으로 사용자가 보다 손쉽게 접근할 수 있는 ALE기법을 이용하여 잠수함 액화산소탱크를 대상으로 수중폭발해석 방식을 제안하고자 하였다.

• Nuclear Engineering and Technology
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• 제56권7호
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• pp.2881-2892
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• 2024

Annular flow refers to a special type of two-phase flow pattern in which liquid flows as a thin film at the periphery of a pipe, tube, or conduit, and gas with relatively high velocity flows at the center of the flow section. This gas also includes dispersed liquid droplets. The liquid film flow rate continuously changes inside the tube due to two processes-entrainment and deposition. To determine the liquid holdup, pressure drop, the onset of dryout, and heat transfer characteristics in annular flow, it is important to have proper knowledge of flow characteristics. Especially a better understanding of entrainment fraction is important for the heat transfer and safe operation of two-phase flow systems operating in an annular two-phase flow regime. Therefore, the objective of this work is to develop a computational model for the simulation of the annular two-phase flow regime and assess the various existing models for the entrainment rate. In this work, Computational Fluid Dynamics (CFD) in ANSYS FLUENT has been applied to determine annular flow characteristics such as liquid film thickness, film velocity, entrainment rate, deposition rate, and entrainment fraction for various gas-liquid flow conditions in a vertical upward tube. The gas core with droplets was simulated using the Discrete Phase Model (DPM) which is based on the Eulerian-Lagrangian approach. The Eulerian Wall Film (EWF) model was utilized to simulate liquid film on the tube wall. Three different models of Entrainment rate were implemented and assessed through user-defined functions (UDF) in ANSYS. Finally, entrainment for fully developed flow was determined and compared with the experimental data available in the literature. From the simulations, it was obtained that the Bertodano correlation performed best in predicting entrainment fraction and the results were within the ±30 % limit when compared to experimental data.

• 한국연소학회:학술대회논문집
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• 한국연소학회 1999년도 제19회 KOSCO SYMPOSIUM 논문집
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• pp.139-148
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• 1999

In oder to analyze the effect of operating conditions on pulverized coal combustion, a numerical study is conducted at the pulverized coal combustor. Eulerian approach is used for the gas phase, whereas Lagrangian approach is used for the particle phase. Turbulence is modeled using standard ${\kappa}-{\varepsilon}$ model. The description of species transport and combustion chemistry is based on the mixture fraction/probability density function(PDF) approach. Radiation is modeled using P-l model. The turbulent dispersion of particles is modeled using discrete random walk model. Swirl number of secondary air affects the flame front, particle residence time and carbon conversion. Primary/Secondary air mass ratio also affects the flame front but little affects the carbon conversion and particle residence time. Air-fuel ratio only affects the flame front due to lack of oxygen. Radiation strongly affects the flame front and gas temperature distribution because pulverized coal flame of high temperature is considered.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2012년도 제45회 KOSCO SYMPOSIUM 초록집
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• pp.355-357
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• 2012

A probability density function (PDF) approach to account for turbulence-chemistry interaction in the context of large eddy simulation (LES) based simulation of scramjets is developed. To solve the high-dimensional joint-composition PDF transport equation robustly, the semi-discrete quadrature method of moments (SeQMOM) is recently proposed [1]. The SeQMOM approach addresses key numerical issues in LES related to the inaccuracies in computing filter-scale gradients, enabling an efficient and numerically consistent solution of the PDF transport equation. The computational tool is used to simulate a cavity-stabilized Mach 2.2 supersonic combustor.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1993년도 한국자동제어학술회의논문집(국내학술편); Seoul National University, Seoul; 20-22 Oct. 1993
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• pp.926-930
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• 1993

An efficient method of formulating the equations of motion of multibody systems is presented. The equations of motion for each body are formulated by using Newton-Eulerian approach in their generic form. And then a transformation matrix which relates the global coordinates and relative coordinates is introduced to rewrite the equations of motion in terms of relative coordinates. When appropriate set of kinematic constraints equations in terms of relative coordinates is provided, the resulting differential and algebraic equations are obtained in a suitable form for computer implementation. The system geometry or topology is effectively described by using the path matrix and reference body operator.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 1997년도 추계 학술대회논문집
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• pp.113-119
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• 1997

This paper addresses to the injection pressure effect on the diesel spray. The injection pressure is varied from 10MPa, in general system, upto 200MPa, in high pressured system in order to understand the effect. The gas phase is modelled in terms of the Eulerian continuum conservation equations of mass, momentum, energy and fuel vapour fraction. The liquid phase is modelled following the discrete droplet model approach in Lagrangian form. The droplet distributions, vapor fractions and gas flows are analyzed in various injection pressure cases.

• Wind and Structures
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• 제20권3호
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• pp.423-448
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• 2015

In this paper the unsteady fluid-structure interaction (FSI) problems with large structural displacement are solved by partitioned solution approaches in the arbitrary Lagrangian-Eulerian finite element framework. The incompressible Navier-Stokes equations are solved by the characteristic-based split (CBS) scheme. Both a rigid body and a geometrically nonlinear solid are considered as the structural models. The latter is solved by Newton-Raphson procedure. The equation governing the structural motion is advanced by Newmark-${\beta}$ method in time. The dynamic mesh is updated by using moving submesh approach that cooperates with the ortho-semi-torsional spring analogy method. A mass source term (MST) is introduced into the CBS scheme to satisfy geometric conservation law. Three partitioned coupling strategies are developed to take FSI into account, involving the explicit, implicit and semi-implicit schemes. The semi-implicit scheme is a mixture of the explicit and implicit coupling schemes due to the fluid projection splitting. In this scheme MST is renewed for interfacial elements. Fixed-point algorithm with Aitken's ${\Delta}^2$ method is carried out to couple different solvers within the implicit and semi-implicit schemes. Flow-induced vibrations of a bridge deck and a flexible cantilever behind an obstacle are analyzed to test the performance of the proposed methods. The overall numerical results agree well with the existing data, demonstrating the validity and applicability of the present approaches.

• Journal of Mechanical Science and Technology
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• 제16권5호
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• pp.683-695
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• 2002

The objective of the present study is to analyze the fluid flow with moving boundary using a finite element method. The algorithm uses a fractional step approach that can be used to solve low-speed flow with large density changes due to intense temperature gradients. The explicit Lax-Wendroff scheme is applied to nonlinear convective terms in the momentum equations to prevent checkerboard pressure oscillations. The ALE (Arbitrary Lagrangian Eulerian) method is adopted for moving grids. The numerical algorithm in the present study is validated for two-dimensional unsteady flow in a driven cavity and a natural convection problem. To extend the present numerical method to engine simulations, a piston-driven intake flow with moving boundary is also simulated. The density, temperature and axial velocity profiles are calculated for the three-dimensional unsteady piston-driven intake flow with density changes due to high inlet fluid temperatures using the present algorithm. The calculated results are in good agreement with other numerical and experimental ones.

• 한국추진공학회지
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• 제15권6호
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• pp.38-46
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• 2011

점화제 주입 특성을 모사할 수 있는 2차원 이상유동의 강내탄도 해석코드 개발하였다. 장약인 추진제의 연소 해석을 위해 Eulerian-Lagrangian 접근법과 LSHUS 기법을 적용하였다. 탄자의 이동에 따른 이동경계면의 해석을 위해 Ghost Cell Extrapolation method를 사용하였다. 개발된 2차원 강내탄도 해석코드는 무차원 강내탄도 해석 코드인 IBHVG2와 기존에 개발된 1차원 강내탄도 해석코드와 비교 검증하였다. 항력식에 따른 이상유동의 비교에서 항력식이 탄자탈출속도의 수치적 해석에 영향을 주는 것을 확인하였다.