• 한국전산유체공학회:학술대회논문집
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• 2010.05a
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• pp.534-541
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• 2010

A high-order accurate Euler flow solver based on a discontinuous Galerkin method has been developed for the numerical simulation of unsteady flows on unstructured meshes. A multi-level solution-adaptive mesh refinement/coarsening technique was adopted to enhance the resolution of numerical solutions efficiently by increasing mesh density in the high-gradient region. An acoustic wave scattering problem was investigated to assess the accuracy of the present discontinuous Galerkin solver, and a supersonic flow in a wind tunnel with a forward facing step was simulated by using the adaptive mesh refinement technique. It was shown that the present discontinuous Galerkin flow solver can capture unsteady flows including the propagation and scattering of the acoustic waves as well as the strong shock waves.

• 한국전산유체공학회:학술대회논문집
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• 2010.05a
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• pp.341-346
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• 2010

In this paper, viscous flow calculation of pump-jet that is used as underwater propulsor was made by using RANS equation. For the validation, calculation for DTRC4119 marine propeller was made and reasonable agreements were obtained between the present results and the experiment. An unstructured overset mesh technique is used for analysis of relative motion between rotor and stator in pump-jet propulsor. Results for pump-jet propulsor were compared with computational results of another researcher.

• 한국전산유체공학회:학술대회논문집
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• 2004.10a
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• pp.79-82
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• 2004

As an alternative numerical method, the lattice Boltzmann method (LBM) is used to simulate a 2-dimensional pressure driven microchannel flow which comes from frequently in MEMS problems. The flow is assumed to be isothermal ideal gas flow. The flow field is calculated with various Knudsen numbers, pressure ratios and aspect ratios of the microchannel. The LBM can show the fundamental characteristics in microchannel flow such as velocity slip and nonlinear pressure drop.

• Journal of computational fluids engineering
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• v.5 no.2
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• pp.28-37
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• 2000

An integrated grid generation has been developed for a Navier-Stokes simulation of flow fields inside multistaged turbomachinery The internal grids are generated by the combination of algebraic and elliptic methods. The interactive mode of the present system is coupled efficiently with the design results and flow solvers. Application to several types of axial-flow turbomachines was demonstrated to be reliable and practical as the pre-processor of the computational fluid engineering for gas turbine engines.

• Korean Journal of Optics and Photonics
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• v.6 no.1
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• pp.16-20
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• 1995

We have studied the spectral narrowing characteristics of the tunable Ti:sapphire laser pumped by the second harmonic generation of Nd:YAG laser. Ti:sapphire laser has uniform excitation distribution by both-side end pumping. We have controlled the angle of grating linearly and achieved the continuous selection of wavelength in the broad range from 705 to 835 nm. The output energy of $380{\mu}J$ at 790 nm. the spectral linewidth of $0.13cm_{-1}$ and the beam divergence of 1.2 mrad have been obtained. The wavelength range with power more than 50% of maximum output was 730-825 nm.825 nm.

• 한국전산유체공학회:학술대회논문집
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• 1999.05a
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• pp.90-97
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• 1999

An implicit turbulent flow solver is developed for 2-D unstructured hybrid meshes. Spatial discretization is accomplished by a cell-centered finite volume formulation using an upwind flux differencing. Time is advanced by an implicit backward Euler time stepping scheme. Flow turbulence effects are modeled by the Spalart-Allmaras one equation model, which is coupled with wall function. The numerical method is applied for flows on a flat plate, the NACA 0012 airfoil, and the Douglas 3 element airfoil. The results are compared with experimental data.

• Journal of computational fluids engineering
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• v.14 no.4
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• pp.93-100
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• 2009

The gridless (or meshfree) methods, such as MPS, SPH, FPM an so forth, are feasible and robust for the problems with moving boundary and/or complicated boundary shapes, because these methods do not need to generate a grid system. In this study, a gridless solver, which is based on the combination of moving least square interpolations on a cloud of points with point collocation for evaluating the derivatives of governing equations, is presented for two-dimensional unsteady incompressible Navier-Stokes problem in the low Reynolds number. A MAC-type algorithm was adopted and the Poission equation for the pressure was solved successively in the moving least square sense. Some typical problems were solved by the presented solver for the validation and the results obtained were compared with analytic solutions and the numerical results by conventional CFD methods, such as a FVM.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2005.10a
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• pp.400-403
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• 2005

The sonar sensors can be divided into a piezo type and an electrostatic type according to a principle of an operating system. The electrostatic type of a sonar sensor is used for map building in this paper. If we know the characteristics of sonar sensor, we can derive the ultrasonic pressure equation from an acoustics theory. We, therefore, developed Ultrasonic Pressure Probabilistic Model (UPPM) to consider the sound pressure in the probability updating process. In this paper, we found that the quality of the resulting probability map is considerably improved, through combining the UPPM with the grid-based mapping algorithm.

• Journal of the Korean Vacuum Society
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• v.15 no.3
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• pp.294-300
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• 2006

We fabricated the distributed feedback (DFB) InP/InGaAs/InP grating structures on InP (100) substrates by metal-organic chemical vapor deposition, and their structural properties were investigated by atomic force microscopy and scanning electron microscopy. Self-assembled InAs/InAlGaAs quantum dots (QDs) were grown on the InP/InGaAs/InP grating structures by molecular beam epitaxy, and their optical properties were compared with InAs/InAlGaAs QDs without grating structure. The duty of the grating structures was about 30%. The PL peak position of InAs/InAlGaAs QDs grown on the grating structure was 1605 nm, which was red-shifted by 18 nm from that of the InAs/InAlGaAs QDs without grating structure. This indicates that the formation of InAs/InAlGaAs QDs was affected by the existence of the DFB grating structures.

• Proceedings of the Korea Water Resources Association Conference
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• 2020.06a
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• pp.414-414
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• 2020

고전 천수방정식을 적용한 2차원 도시홍수 모델링에서는 지형의 정확한 반영을 위해 고해상도 격자가 요구되며 이는 많은 계산시간과 노력을 필요로 한다. 최근에는 다공성 천수방정식을 적용한 도시홍수해석으로 많은 계산 노력이 요구되는 도시홍수모델링의 한계를 극복한 연구가 많이 이루어지지고 있다. 이러한 연구는 도시 홍수에서 흐름이 공간적으로 변화할 때 불균일 공극이 존재하므로 격자의 크기를 다르게 하여 이러한 불균일성을 해결하고자 하는 등방성 천수모형의 적용에서 시작되었다. 하지만, 등방성 공극을 고려한 도시홍수 해석모형은 대표요소체적(REV)보다 더 큰 격자의 적용을 해야 하는 제한성을 가진다. 반면, 비등방성 공극은 대표요소체적의 적용이 필요하지 않아 불균일 공극의 크기에 관계없이 이론상으로는 동일한 해상도의 격자가 사용가능하긴 하지만, 실제 도시홍수 해석에서 중요하면서도 도전적인 연구이다. 본 연구에서는 도시홍수의 효율적 계산을 위해 비등방성 공극을 고려한 적분형 다공성 천수방정식을 기반으로 하는 2차원 도시홍수 해석모형을 개발하였다. 모형의 개발을 위해, 적용 격자내에서 도시지역의 건물이 차지하는 길이 및 면적을 산정하고 그 값을 2차원 천수방정식에 적용 가능하도록 체적공극(𝜙_j)와 면적공극(𝜓_k)을 2차원 고전 천수방정식에 추가하였다. 개발모형은 고전 천수방정식, 등방성 공극 고려(미분형 다공성) 천수방정식 및 비등방성 공극 고려(적분형 다공성) 천수방정식의 적용이 가능하여, 각 모형에 적합한 2차원 격자 생성, 각 모형의 매개변수를 보정 그리고 정확성, 효율성, 적용성이 비교 가능하다. 각 모형의 정확성과 효율성 비교를 위해 3가지의 오차 비교 (구조적 오차, 격자크기 오차, 공극 모형 오차), 계산시간 비교, 공간 변동성 검증을 위한 수심 종단형상 비교하였다.