• 한국전산유체공학회:학술대회논문집
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• 2007.04a
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• pp.116-119
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• 2007

In this study the unsteady aerodynamic analysis of a hovering helicopter rotor is performed. For the accurate flow field analysis Euler equations and the free wake method are coupled. The Euler equations are solved to find the pressure distribution around the rotor, and free wake method is used to give the boundary condition for the solution of Euler equations. Also, vortex strength and wake motion after the rotor are simulated by the free wake method. The accuracy of the present method is compared with the source sink model. The present method is applied to the hovering Caradonna-Tung rotor and compared with experimental results.

• Journal of the Korean Society of Propulsion Engineers
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• v.23 no.6
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• pp.1-10
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• 2019

The wave motion inside the nozzle is known as one of the major damping elements of the rocket's combustion instability by it's aeroacoustic effects that result from the flow passage through the nozzle throat. These effects can be quantitatively evaluated by the nozzle admittance. In this study, one-dimensional linearized Euler equation was adopted to calculate the nozzle admittance, and trend analysis was performed depending on the nozzle's main design variables. As a result, when nozzle converging part shortens, it is verified that the frequency dependency of the nozzle admittance is decreased due to the widened frequency range with lowered longitudinal nozzle admittance. Also, admittance estimation using the short nozzle theory is not appropriate when the first tangential mode of the pressure perturbation arises.

• Journal of the korean Society of Automotive Engineers
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• v.11 no.5
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• pp.90-100
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• 1989

본 논문은 이상유동 시스템에 부유도니 슈트, 미분탄과 같은 고 흡수, 방사하는 입자에 의한 열 확산 현상에 대한 복사효과를 수치적으로 검토하였다. 가스, 입자유동의 지배방정식들은 오일러 관점의 two-fluid model 의 근간에서 수행되었으며, 에너지 방정식의 비선형 복사생성항은 P-1 근사방법에 의해 계산되었다. 복사효과가 증가될 때에 열확산적 입자의 벽면에 대한 부착율은 상당히 낮아짐을 보였으며 열확산 현상의 스토크스 수에 따른 효과도 고려되었다.

• Journal of computational fluids engineering
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• v.19 no.2
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• pp.58-65
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• 2014

The adaptive wavelet method is studied for the enhancement of computational efficiency of three-dimensional flows. For implementation of the method for three-dimensional Euler equation, wavelet decomposition process is introduced based on the previous two-dimensional adaptive wavelet method. The order of numerical accuracy of an original solver is preserved by applying modified thresholding value. In order to assess the efficiency of the proposed algorithm, the method is applied to the computation of flow field around ONERA-M6 wing in transonic regime with 4th and 6th order interpolating polynomial respectively. Through the application, it is confirmed that the three-dimensional adaptive wavelet method can reduce the computational time while conserving the numerical accuracy of an original solver.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.8
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• pp.8-17
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• 2005

It is well known that preconditioning methods are efficient for convergence acceleration in the compressible low Mach number flows. In this study, the original Euler equations and three differently nondimensionalized preconditioning methods are implemented in two dimensional inviscid bump flows using the 3rd order MUSCL and DADI schemes as numerical flux discretization and time integration, respectively. The multigrid and local time stepping methods are also used to accelerate the convergence. The test case indicates that a properly modified local preconditioning technique involving concepts of a global preconditioning allows Mach number independent convergence. Besides, an asymptotic analysis for properties of preconditioning methods is added.

• Proceedings of the Korea Water Resources Association Conference
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• 2017.05a
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• pp.292-292
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• 2017

하천에서 주로 부유사의 형태로 이송되는 유사는 크게 점착성 유사와 비점착성 유사로 구분된다. 입자의 크기가 약 $63{\mu}m$이하인 유사는 입자 표면의 전자기적 점착력의 영향이 우세하여 유사입자들은 지속적인 응집현상을 겪는다. 응집 현상을 통해 유사의 가장 단위인 일차입자(Primary Particle)들은 하나의 커다란 덩어리인 플럭(Floc)을 형성한다. 응집현상이 중요한 이유는 형성된 플럭의 크기 및 밀도가 끊임없이 변화하는 데 있다. 크기와 밀도의 지속적인 변화로 인하여 유사의 부유에 직접적으로 관계하는 침강속도가 변화한다. 우리나라의 금강 및 낙동강의 하구는 점착성 유사가 지배적인 환경으로, 하구에서의 유사 이동을 살펴보기 위해서는 흐름 방향 및 연직방향으로의 흐름 특성(Hydrodynamics)변화와 응집 모형을 통한 응집 현상의 고려가 필수적이다. 이에따라, 본 연구에서는 흐름 방향 및 연직방향으로의 2차원 점착성 유사 이동모형에 관한 개념적 틀(Framework)을 제시한다. 2차원 점착성 유사 이동 모형의 개념적 틀은 기존의 1차원 연직 점착성 유사 이동 모형을 근간으로 한다. 모형에서 흐름을 구성하는 지배 방정식은 오일러-오일러 이상방정식(Eulerian-Eulerian Two-Phase Equation)을 통해 얻는다. 유사상(Sediment Phase, Dispersed Phase)와 유체상(Fluid Phase, Continuous Phase)는 혼합물 이론(Mxiture Theory)를 통해 하나의 혼합물 상(Mixture Phase)의 지배방정식으로 대표된다. 난류의 계산은 와점성 모형 중 -${\varepsilon}$모형을 통해 수행되며, 부유사의 농도는 유사의 이송-확산 방정식을 통해 모의된다. 입력된 흐름 조건을 따라 초기 흐름이 모의되면, 유체 내에서 시간에 따른 플럭의 크기가 계산된다. 플럭의 크기가 계산되는 과정에서 밀도와 침강 속도가 계산되며, 그 이후에 유체 내 유사의 농도가 계산된다. 난류 모의가 수행되고 난 이후에, 유속이 재계산 된다. 이러한 과정을 통해 흐름 방향 및 연직 방향으로의 유사 이동 모의가 가능한 2차원 점착성 유사 이동 모형이 개발될 수 있을 것이라고 생각된다.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.35 no.7
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• pp.677-683
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• 2011

Until now, several empirical models for assessing the damage due to TNT explosions have been proposed. A set of analytical solutions for the time-dependent radius of an expanding fire-ball after detonation of TNT was obtained by solving the continuity, Euler (momentum), and energy equations with a "polytrope" assumption at the fire-ball center. The shock waves developed from the rapid expansion of a fire-ball under water were obtained by using the KirkwoodBBethe hypothesis. The calculated period of bubble oscillation and the maximum radius of the bubble resulting from the fire-ball due to a violent underwater TNT explosion were in good agreement with the experimental data.

• Journal of computational fluids engineering
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• v.4 no.2
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• pp.67-73
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• 1999

In the present paper, three types of the flow solvers were used to investigate the influence on the airfoil shape optimization. The adopted equations, i.e., Euler, thin layer Navier-Stokes and full Navier-Stokes ones. are solved using implicit LU-ADI decomposition scheme. The gradient projection method with the sinusoidal function was used as an optimization algorithm. The present numerical method was applied to the drag minimization problems under the initial shape of NACA0012 airfoils.

• Journal for History of Mathematics
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• v.17 no.4
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• pp.133-152
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• 2004

In this paper, we discuss students' conceptual development of eigen value and eigen vector in differential equation course based on reformed differential equation using the mathematical model of mass spring according to historico-generic principle. Moreover, in setting of small group interactive learning, we investigate the students' development of mathematical attitude.

• 한국전산유체공학회:학술대회논문집
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• 1999.05a
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• pp.171-176
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• 1999

In the present paper, three types of the flow solvers were used to investigate the influence on the airfoil shape optimization. The adopted equations, i.e., Euler , thin layer Navier- Stokes and full Navier-Stokes ones, are solved using implicit LU-ADI decomposition scheme. The feasible direction algorithm with the sinusoidal function was used as an optimization algorithm. The present numerical method was applied to the drag minimization problems under the initial shape of NACA0012 airfoils.