• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1994.04a
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• pp.51-55
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• 1994

탄성체 동역학 해석에 있어서 변형을 나타내기 위해 사용되는 좌표로는 크게 절점좌표와 모우드좌표로 구분된다. 상대적으로 적은 좌표수를 사용하는 모우드좌표가 기계나 항공, 우주 분야에선 일반적으로 많이 사용된다. 그러나, 모우드를 선정함에 있어서의 기준의 불확실함 등으로 인해, 모우드좌표는 많은 경험을 요구하게 된다. 모우드좌표에 비해 많은 시간이 걸리지만, 절점 좌표의 사용은 누구나 쉽게 사용할 수 있음을 장점으로 한다. 본 연구에서는 두 가지 좌표로 탄성체 동역학의 운동방정식을 유도한 뒤, 슬라이더-크랭크 기구의 해석을 수행하여 그 결과를 서로 비교해 보고자 한다.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2003.10a
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• pp.239-239
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• 2003

• Transactions of the Korean Society of Mechanical Engineers A
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• v.24 no.1 s.173
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• pp.94-102
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• 2000

A computer program for three dimensional dynamic analysis of a mount system composed of rigid or flexible bodies and mount elements is developed. Cartesian coordinates and Euler parameters are used to specify the positions and orientations of the bodies. The equations of motion are formulated using Langrange equation and Langrange multiplier technique. The developed program includes routine, for inclined mount elements, several kinds of driving constrains, and external forces. The Static equilibrium analysis routine is also developed using iterative method.

• Proceedings of the Computational Structural Engineering Institute Conference
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• 2011.04a
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• pp.127-130
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• 2011

본 연구에서는 나노입자와 고분자 기지 간에 공유결합을 형성시킨 나노복합재의 계면특성과 탄성계수에서 나타나는 크기효과를 고려하기 위해 분자동역학과 미시역학모델을 순차적으로 연계하는 멀티스케일 해석모델을 제안하였다. 나노입자의 체적분율이 동일한 5개의 나노복합재 셀에 대해, 입자의 표면 원자와 고분자 기지 간에 탄소로 구성된 공유결합을 생성시킨 후 분자동 역학 전산모사를 통해 탄성계수를 예측하였고, 공유결합이 존재하지 않는 나노복합재의 탄성계수와 이를 비교하여 계면의 물성증가와 탄성계수에서 나타나는 입자의 크기효과를 규명하였다. 향상된 계면의 특성을 연속체 해석 모델에서 고려하기 위해 분자동역학 해석결과와 미시역학 모델을 연계하는 순차적 브리징 기법을 적용하였고, 이로부터 계산된 계면의 물성의 타당성을 유한요소 해석을 통해 검증하였다. 그 결과 입자와 기지 간 공유결합을 통해 나노복합재가 보다 넓은 범위에 걸친 크기효과를 나타냈으며, 제안된 브리징 모델을 통해서 물리적으로 타당한 계면의 탄성계수 값을 계산할 수 있었다.

• Journal of the Korean Society for Precision Engineering
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• v.21 no.5
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• pp.114-121
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• 2004

Recently, the finite element absolute nodal coordinate formulation (ANCF) was developed for the large deformation analysis of flexible bodies in multi-body dynamics. This formulation is based on the finite element procedures and the general continuum mechanics theory to represent the elastic forces. In this paper, a computation method of dynamic stress in flexible multi-body dynamics using absolute nodal coordinate formulation is proposed. Numerical examples, based on an Euler-Bernoulli beam theory, are shown to verify the efficiency of the proposed method. This method can be applied for predicting the fatigue life of a mechanical system. Moreover, this study demonstrates that structural and multi-body dynamic models can be unified in one numerical system.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.38 no.2
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• pp.115-120
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• 2014

In this study, a module is developed for modeling and analyzing dynamic behavior of a wind turbine using RecurDyn, which is a commercial multi-body dynamics software developed by FunctionBay, Inc. The wind turbine consists of tower, nacelle, hub and blades. Tower and blades are regarded as flexible bodies for considering elastic effect using beam theory and spring force. In this paper, a constant speed wind was assumed and aerodynamic force is modeled using BEM theory. Dynamic analysis applying this aerodynamic force is carried out. To verify the validity of analysis results, these results are compared to those of GH-Bladed which is a commercial software for analyzing wind turbine system distributed by Garrad Hassan.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.36 no.12
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• pp.1489-1495
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• 2012

In this study, we perform the structural analysis of a floating offshore wind turbine tower by considering the dynamic response of the floating platform. A multibody system consisting of three blades, a hub, a nacelle, the platform, and the tower is used to model the floating wind turbine. The blades and the tower are modeled as flexible bodies using three-dimensional beam elements. The aerodynamic force on the blades is calculated by the Blade Element Momentum (BEM) theory with hub rotation. The hydrostatic, hydrodynamic, and mooring forces are considered for the platform. The structural dynamic responses of the tower are simulated by numerically solving the equations of motion. From the simulation results, the time history of the internal forces at the nodes, such as the bending moment and stress, are obtained. In conclusion, the internal forces are compared with those obtained from static analysis to assess the effects of wave loads on the structural stability of the tower.

• New & Renewable Energy
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• v.7 no.4
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• pp.50-57
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• 2011

A wind turbine simulation program for the coupled dynamics of aerodynamics, elasticity, multi-body dynamics and controls of turbine is newly developed by combining an aero-elastic code and a multi-body dynamics code. The aero-elastic code, based on the blade momentum theory and generalized dynamic wake theory, is developed by NREL(National Renewable Energy Laboratory, USA). The multi-body dynamics code is commercial one which is capable of accounting for geometric nonlinearity and twist deflection. A turbulent wind load case is simulated for the NREL 5-MW baseline wind turbine model by the developed program and FAST. As a result, the two results agree well enough to verify the reliability of the developed program.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.29 no.6
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• pp.577-582
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• 2016

In this study, a multiscale method for solving a thermoelasticity problem for interphase in the polymeric nanocomposites is developed. Molecular dynamics simulation and finite element analysis were numerically combined to describe the geometrical boundaries and the local mechanical response of the interfacial region where the polymer networks were highly interacted with the nanoparticle surface. Also, the micrmechanical thermoelasticity equations were applied to the obtained equivalent continuum unit to compute the growth of interphase thickness according to the size of nanoparticles, as well as the thermal phase transition behavior at a wide range of temperatures. Accordingly, the equivalent continuum model obtained from the multiscale analysis provides a meaningful description of the thermoelastic behavior of interphase as well as its nanoparticle size effect on thermoelasticity at both below and above the glass transition temperature.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.30 no.8
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• pp.46-55
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• 2002

A nonlinear aeroelastic analysis system in transonic and supersonic flows has been developed using high speed parallel processing technique on the network based PC-clustered machines. This paper includes the coupling of advanced numerical techniques such as computational structural dynamics (CSD), finite element method (FEM) and computational fluid dynamics (CFD). The unsteady Euler solver on dynamic unstructured meshes is employed and coupled with computational aeroelastic solvers. Thus it can give very accurate engineering data in the structural and aeroelastic design of flight vehicles. To show the great potential of useful application, transonic and supersonic flutter analyses have been conducted for a complete aircraft model under developing in Korea.