• 대한기계학회논문집A
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• 제30권10호
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• pp.1235-1241
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• 2006

A new hydrocode which is still under development using Lagrangian, Eulerian and arbitrary Lagrangian-Eulerian operators, has been described. The three operators are implemented into a single framework by incorporating the sequential three stages of Lagrangian, remesh and remap stages. Several numerical schemes used for each operator are discussed briefly in this paper. In order to evaluate the characteristics of each operator, the Taylor Impact Test has been simulated using each operator and the results are compared. Currently the code is 1st order accuracy in the material interface tracking algorithm and can not handle multimaterial in the mixed cell. The areas of possible enhancement of the code are also discussed.

• 대한조선학회논문집
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• 제54권6호
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• pp.470-475
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• 2017

Since the intake air of gas turbine engine of marine purpose contains water particles, inertial separator for separating the air and water particles are provided. Saw type and wave type separator are now used to separate inflow water particle from the gas. In this paper, the design parameters of saw type separator are studied by numerical simulations. Using the commercial CFD program, Star-CCM+, Lagrangian-Eulerian method was used to perform the analysis of two phase flow of the mist in the air. This method solves Reynolds-Averaged Navier-Stokes equations in Eulerian framework for the continuous phase, while solves equation of motion for individual particles in Lagrangian framework. Lagrangian multiphase method was applied to monitor the particles of different sizes and shapes and to verify collision between particles by chasing particles. Water particles were injected through injectors located at the inlet of the separator and escape mode was used which assumes that the particles attached on the surface of inertial separator were removed from the simulation, effectively escaping the solution domain. Through the numerical computations with the inlet condition of constant water particle size in the wetness fraction of 85%, efficiency of eliminating the water particle and the pressure drop between the inlet and outlet were examined.

• 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.

• 한국입자에어로졸학회지
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• 제13권4호
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• pp.173-182
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• 2017

An Eulerian-Lagrangin approach is used to compute particle dispersion from a power plant chimney. For air flow, three-dimensional incompressible filtered Navier-Stokes equations are solved with a subgrid-scale model by integrating the Newton's equation, while the dispersed phase is solved in a Lagrangian framework. The velocity ratios between crossflow and a jet of 0.455 and 0.727 are considered. Flow fields and particle distribution of both cases are evaluated and compared. When the velocity ratio is 0.455, it demonstrates a Kelvin-Helmholtz vortex structure above the chimney caused by the interaction between crossflow and a jet, whereas the other case shows flow structures at the top of the chimney collapsed by fast crossflow. Also, complex wake structures cause different particle distributions behind the chimney. The case with the velocity ratio of 0.727 demonstrates strong particle concentration at the vortical region, whereas the case with the velocity ratio of 0.455 shows more dispersive particle distribution. The simulation result shows similar tendency to the experimental result.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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• pp.664-671
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• 2017

수직 발사대는 발사체에서 나오는 화염에 의하여 구조체의 손상이 일어날 수 있고 특히 후방덮개는 화염에 의하여 직접적으로 변형이 일어나므로 이를 해석하기 위해서는 유체-고체 연성해석 기법을 필요로 한다. 본 연구에서 발사체의 화염은 Eulerian 기법을 이용하여 해석하였고, 발사대의 후방 덮개는 Lagrangian 기법을 사용하여 해석하였다. 서로 다른 두 물질간의 경계면은 레벨을 통하여 추적을 하였고 경계면에서의 경계값은 가상유체 기법을 활용하여 결정하였다. 본 논문에서는 후방 덮개의 변형 형상에 따라 달라지는 유동의 변화를 확인하였다.

• 정보처리학회논문지A
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• 제16A권6호
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• pp.419-426
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• 2009

일반적으로 사실성 있는 유체를 시뮬레이션하기 위해 Navier-Stokes 방정식을 사용한다. Euler 구조에서 Navier-Stokes 방정식을 풀 때, 이 류항은 비선형이어서 계산이 복잡하기 때문에 근사화한 모델로 Semi-Lagrangian 방법을 사용한다. Semi-Lagrangian 방법에서는 먼저 이류하 는 위치를추적하고, 추적한 위치에서 값을 보간해서 사용한다. Stam이 제안한 방법으로 계산할 경우, 이 과정에서 수치적 소실이 많이 발생하 기 때문에 수치적 소실을 보정하려는 노력들이 있어 왔다. 그러나 대부분의 경우에 보간하는 과정에서의 소실을 줄이려는 노력이거나, 입자를 같이 사용하는 방법이었다. 따라서 본 논문에서는 Euler 구조에서 다른 추가나 변형을 가하지 않고 이류항의 연산에서 추적법을 개선함으로 수 치적 소실을 줄이는 방법을 제안한다. 우리의 방법에서는 현재 격자의 속도로 역추적하는 기존의 방법이 아니라, 현재의 격자로 오게 될 속도 를 가진 격자를 찾아서, 그 격자의 물리량들을 선형 보간하여 사용한다. 이는 직관적으로 생각할 때, 어느 지점의 물리량은 그 지점의 속도로 인해 다음 단계에 다른 지점에 있게 된다는 사실을 그대로 적용한 것이다. 본 논문에서 제안한 방법으로 기체를 시뮬레이션 했을 때 수치적 소 실이 줄었으며, 그로 인해 사실성을 높이면서도 실시간 처리가 가능했다.

• Structural Engineering and Mechanics
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• 제32권2호
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• pp.283-300
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• 2009

The characteristic response of a structure to blast load may be divided into two distinctive phases, namely the direct blast response during which the shock wave effect and localized damage take place, and the post-blast phase whereby progressive collapse may occur. A reliable post-blast analysis depends on a sound understanding of the direct blast effect. Because of the complex loading environment and the stress wave effects, the analysis on the direct effect often necessitates a high fidelity numerical model with coupled fluid (air) and solid subdomains. In such a modelling framework, an appropriate representation of the blast load and the high nonlinearity of the material response is a key to a reliable outcome. This paper presents a series of calibration study on these two important modelling considerations in a coupled Eulerian-Lagrangian framework using a hydrocode. The calibration of the simulated blast load is carried out for both free air and internal explosions. The simulation of the extreme dynamic response of concrete components is achieved using an advanced concrete damage model in conjunction with an element erosion scheme. Validation simulations are conducted for two representative scenarios; one involves a concrete slab under internal blast, and the other with a RC column under air blast, with a particular focus on the simulation sensitivity to the mesh size and the erosion criterion.

• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 2008년도 춘계학술대회 논문집
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• pp.235-237
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• 2008

A unified hydrocode, ExLO, in which Largrangian, ALE and Eulerian solvers are incorporated into a single framework, has recently been developed in Korea. It is based on the three dimensional explicit finite element method and written in C++. ExLO is mainly designed for the calculation of structural responses to highly transient loading conditions, such as high-speed impacts, high-speed machining, high speed forming and explosions. In this paper the numerical schemes are described. Some improvements of the material interface and advection scheme are included. Details and issues of the momentum advection scheme are provided. In this paper the modeling capability of ExLO has been described for two extreme loading events; high-speed impacts and explosions. Numerical predictions are in good agreement with the existing experimental data. Specific applications of the code are discussed in a separate paper in this journal. Eventually ExLO will be providing an optimum simulation environment to engineering problems including the fluid-structure interaction problems, since it allows regions of a problem to be modeled with Lagrangian, ALE or Eulerian schemes in a single framework.

• Nuclear Engineering and Technology
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• 제51권5호
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• pp.1261-1271
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• 2019

Droplet size and distribution are important parameters determining venturi scrubber performance. In this paper, we proposed physical models for a maximum stable droplet size prediction and upper limit log-normal (ULLN) distribution parameters. For the proposed maximum stable droplet size prediction model, a Eulerian-Lagrangian framework and a Reitz-Diwakar breakup model are solved simultaneously using CFD calculations to reflect the effect of multistage breakup and droplet acceleration. Then, two ULLN distribution parameters are suggested through best fitting the previously published experimental data. Results show that the proposed approach provides better predictions of maximum stable droplet diameter and Sauter mean diameter compared to existing simple empirical correlations including Boll, Nukiyama and Tanasawa. For more practical purpose, we developed the simple, one dimensional (1-D) calculation of Sauter mean diameter.

• 한국항공우주학회지
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• 제44권11호
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• pp.957-964
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• 2016

본 연구에서는 발사체를 보관하고 사출하는 수직 발사대에서 발사체의 화염에 의해 변형되는 발사대 후방덮개의 응답을 유체-고체 연성해석 기법을 이용하여 해석하였다. 발사체의 화염은 Eulerian 기법을 이용하여 해석하였고, 탄소성 변형이 일어나는 후방 덮개는 9절점 유한 요소 기법을 사용하여 해석하였다. 유체와 고체 물질간의 경계면 추적은 레벨 셋 기법을 사용하였고 경계값은 가상유체 기법을 이용하여 결정하였다. 각 해석 기법들은 이론값들을 통하여 검증되었고, 후방 덮개의 해석 결과는 후방 덮개가 변형되는 시간을 비교하였다.