• International Journal of Naval Architecture and Ocean Engineering
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• 제6권4호
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• pp.1024-1040
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• 2014

The theoretical background and a numerical solution procedure for a time domain hydroelastic code are presented in this paper. The code combines a VOF-based free surface flow solver with a flexible body motion solver where the body linear elastic deformation is described by a modal superposition of dry mode shapes expressed in a local floating frame of reference. These mode shapes can be obtained from any finite element code. The floating frame undergoes a pseudo rigid-body motion which allows for a large rigid body translation and rotation and fully preserves the coupling with the local structural deformation. The formulation relies on the ability of the flow solver to provide the total fluid action on the body including e.g. the viscous forces, hydrostatic and hydrodynamic forces, slamming forces and the fluid damping. A numerical simulation of a flexible barge is provided and compared to experiments to show that the VOF-based flow solver has this ability and the code has the potential to predict the global hydroelastic responses accurately.

• 대한전자공학회논문지TC
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• 제44권7호통권361호
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• pp.96-104
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• 2007

본 논문에서는 필드 솔버와 회로 시뮬레이션을 통한 온 칩 인덕터의 패드 및 주변 그라운드의 디임베드 방법을 설명하였으며, 필드 솔버의 결과와 회로 시뮬레이션을 통한 디임베드 방법은 각각 측정 결과와 메트리스 연산 결과와 비교하여 검증하였다. 또한 디임베드 된 인덕터의 모델을 적용한 LNA 설계하고 제작하였으며 제작한 LNA의 결과는 측정 결과와 비교하여 디임베드를 적용하였을 때 2.5GHz 이상의 대역에서 보다 측정치에 접근함을 확인하였다. 본 논문에서 제시한 회로 시뮬레이션을 통한 디임베드 방법은 다른 수동 온칩 소자의 소자값을 얻는 데 손쉽게 사용될 수 있는 방법이며 이를 적용하여 보다 정확한 RFIC(radio frequency integrated circuit) 회로 설계가 가능할 것으로 사료된다.

• International Journal of Naval Architecture and Ocean Engineering
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• 제13권1호
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• pp.433-449
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• 2021

In this study, a newly enhanced Fluid-Structure Interaction (FSI) model which incorporates mooring lines was used to simulate a floating structure. The model has two parts: a Computational Fluid Dynamics (CFD) model and a mooring model. The open-source CFD OpenFOAM® v1712 toolbox was used in the present study, and the convergence criteria and relaxation method were added to the computational procedure used for the OpenFOAM multiphase flow solver, interDyMFoam. A newly enhanced, tightly coupled solver, CoupledinterDyMFoam, was used to decrease the artificial added mass effect, and the results were validated through a series of benchmark cases. The mooring model, based on the finite element method, was established in MATLAB® and was validated against a benchmark analytical elastic catenary solution and numerical results. Finally, a model which simulates a floating structure with mooring lines was successfully constructed by connecting the mooring model to CoupledinterDyMFoam.

• Wind and Structures
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• 제23권5호
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• pp.421-447
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• 2016

Wind-induced and earthquake-induced excitations on tall structures can be effectively controlled by Tuned Liquid Damper (TLD). This work presents a numerical simulation procedure to study the performance of tuned liquid tank- structure system through ${\sigma}$-transformation based fluid-structure coupled solver. For this, a 'C' based computational code is developed. Structural equations are coupled with fluid equations in order to achieve the transfer of sloshing forces to structure for damping. Structural equations are solved by fourth order Runge-Kutta method while fluid equations are solved using finite difference based sigma transformed algorithm. Code is validated with previously published results. The minimum displacement of structure is observed when the resonance condition of the coupled system is satisfied through proper tuning of TLD. Since real-time excitations are random in nature, the performance study of TLD under random excitation is also carried out in which the Bretschneider spectrum is used to generate the random input wave.

• International Journal of Aeronautical and Space Sciences
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• 제10권1호
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• pp.104-111
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• 2009

An unstructured overset mesh method has been developed for the simulation of unsteady flow fields around isolated rotors and rotor-fuselage configurations. The flow solver was parallelized for the efficient calculation of complicated flows requiring a large number of cells. A quasi-unsteady mesh adaptation technique was adopted to enhance the spatial accuracy of the solution and to better resolve the rotor wake. The method has been applied to calculate the flow fields around rotor-alone and rotor-fuselage configurations in forward flight. Validations were made by comparing the predicted results with those of measurements. It was demonstrated that the present method is efficient and robust for the prediction of unsteady time-accurate flow fields involving multiple bodies in relative motion.

• 한국전산유체공학회지
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• 제16권1호
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• pp.36-41
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• 2011

Numerical simulation of air-launched rockets from a helicopter was conducted to investigate the aerodynamic interference between air-launched rocket and helicopter. For this purpose, a three-dimensional inviscid flow solver has been developed based on unstructured meshes. An overset mesh technique was used to describe the relative motion between rocket and rocket launcher. The flow solver was coupled with six degree-of-freedom equation to predict the trajectory of free-flight rockets. For the validation, calculations were made for the impinging jet with inclined plate. The rotor downwash of helicopter was calculated and applied to simulation of air-launched rocket. It is shown that the rotor downwash has non-negligible effect on the air-launched rocket and its plume development.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2006년도 PARALLEL CFD 2006
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• pp.27-34
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• 2006

In this paper, a recently proposed parallel hybrid particle-continuum (DSMC-NS) scheme employing 3D unstructured grid for solving steady-state gas flows involving continuum and rarefied regions is described [1]. Substitution of a density-based NS solver to a pressure-based one that greatly enhances the capability of the proposed hybrid scheme and several practical experiences of implementation learned from the development and verifications are highlighted. At the end, we present some simulation results of a realistic RCS nozzle plume, which is considered very challenging using either a continuum or particle solver alone, to demonstrate the capability of the proposed hybrid DSMC-NS method.

• 한국HCI학회:학술대회논문집
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• 한국HCI학회 2009년도 학술대회
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• pp.463-468
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• 2009

본 논문은 데스크탑 PC 에서만 구현 가능하였던 기존의 유체 시뮬레이션 기술을 모바일 환경으로 확장하는 방법론을 제시한다. 유체 시뮬레이션은 나비어-스토크스 (Navier-Stokes) 방정식의 수치적 해를 구하는 것이며, 기존의 방법론은 수치적 해의 안정성과 [1] 사실성 [2]에 그 초점을 맞추고 있다. 하지만 이는 모바일 기기에서 기대하기 힘든 충분한 연산 자원을 가정한 것이다. 한편, 모바일 환경에서의 물리기반 기술은 현재 강체 시뮬레이션 모듈이 주로 활용되고 있으며 [3], 유체 시뮬레이션은 높이장 (Height field) 기반의 단순한 모델만이 제시되어있다 [4]. 이를 극복하기 위해 본 연구에서는 이러한 한계를 극복한 수정된 비압축유동의 시뮬레이션 기법을 소개하며, 또한 모바일 상에서 유체의 가시화 기술을 제안한다.

• 대한전자공학회논문지SD
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• 제44권5호
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• pp.42-49
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• 2007

본 논문에서는 열전도 환경하의 MCM과 진공에서 작동하는 우주전자 장비의 신뢰도 최적화를 위한 부품 배치 연구에 관해 기술하고 있다. 최적배치를 위해 초기 부품 배치 후 FDM을 solver로 이용하여 부품의 접합온도를 계산하였으며 접합온도를 이용하여 전자장치의 신뢰도를 예측한 후 시뮬레이티드 어닐링 방법을 통해 신뢰도 최적배치 결과가 기술되었다. 시뮬레이티드 어닐링 적용 시 흔들기는 부품 치환방식을 이용하였으며 온도 감소계수 및 열 평형 계수의 변화에 따른 시뮬레이션 결과를 기술하였으며 특히 장치의 고장률 최소화 목적함수와 평균 접합온도 최소화 목적함수에 대해 각 적용결과에 대한 비교분석을 통하여 새로운 신뢰도 최적화 접근방법을 제안하였다.

• 한국정보과학회:학술대회논문집
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• 한국정보과학회 2008년도 한국컴퓨터종합학술대회논문집 Vol.35 No.1 (A)
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• pp.72-73
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• 2008