• Journal of the Korean Society for Railway
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• v.13 no.1
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• pp.16-22
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• 2010

Various programs for dynamic simulation of the railway vehicle have advantages and disadvantages. These programs have limitation that cannot express a large deformable body for an wire of the railway vehicle. In this study, a program for dynamic simulation of the railway vehicle is developed. And the rigid, flexible and large deformable body can be simulated using this program. Its reliability is verified by comparison with a commercial program. Also, a wire is considered as the large deformable body and a sliding joint which connects the rigid body to the large deformable body is included. Moreover, as the wheel-rail contact module is added, the dynamic simulation of the railway vehicle can be analyzed using the developed program.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2002.04a
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• pp.29-30
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• 2002

본 연구에서는 Boeing사에서 개발한 EASY5 프로그램을 이용하여 터보팬 엔진을 모델링하고 성능해석을 수행하였다. 연구대상 엔진인 BR715-56 엔진은 추력이 20,000lbf급인 2 스풀 터보팬 엔진으로 분리흐름(Separate Flow) 형이다. 엔진은 팬, 압축기, 연소기, 저압터어빈, 압축기터어빈, 팬 노즐 및 Core 노즐로 구성되어 있으며 Station No.는 Fig 1과 같다. 연구에 사용된 EASY5 프로그램은 동역학 시스템을 모델링하고 해석하는 프로그램으로, 제공되는 라이브러리 구성품을 이용하여 보다 쉽게 동적 시스템을 모델링할 수 있다. 또한 Steady-State Solver를 이용하여 정적 평형상태를 빠른 시간에 찾을 수 있어 보다 빠른 해석을 수행할 수 있다. 또한 해석된 동역학 모델을 FORTRAN이나 C 코드로 생성하여 제공함으로써 프로그램의 수정이나 보완이 용이하고, 제공되지 않은 시스템의 라이브러리 구성품의 경우에는 사용자 정의 코드를 만들어 사용함으로써 프로그램의 기능을 확장할 수 있다. EASy5는 대표적인 제어기 설계 소프트웨어인 MATLAB, MATRIX-x와의 호환도 가능하며 NASTRAN등과 같은 유한요소 해석 프로그램과의 데이터 공유도 가능하여 보다 폭 넓은 시스템 모델링과 제어기 설계도 쉽게 할 수 있다.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.38 no.1
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• pp.17-23
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• 2014

Graphics processing units (GPUs) are ideal for solving problems involving parallel data computations. In this study, the GPU is used for effectively carrying out a multi-body dynamic simulation with particle dynamics. The Hilber-Hushes-Taylor (HHT) implicit integration algorithm is used to solve the integral equations. For detecting collisions among particles, the spatial subdivision algorithm and discrete-element methods (DEM) are employed. The developed program is verified by comparing its results with those of ADAMS. The numerical efficiencies of the serial program using the CPU and the parallel program using the GPU are compared in terms of the number of particles, and it is observed that when the number of particles is greater, more computing time is saved by using the GPU. In the present example, when the number of particles is 1,300, the computational speed of the parallel analysis program is about 5 times faster than that of the serial analysis program.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.19 no.3 s.73
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• pp.295-302
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• 2006

In this study, computational structural dynamic analyses of a gyrocopter have been conducted considering unsteady dynamic hub-loads due to rotating blades. 3D CATIA models with detailed mechanical parts we constructed and virtually assembled into the complete aircraft configuration. The dynamic loading generated by rotating blades in the forward flight condition are calculated by a commercial computational fluid dynamics (CFD) code such as FLUENT. Modal based transient and frequency response analyses are used to efficiently investigate vibration characteristics of the gyrocopter. Free vibration analysis results for different fuel and pilot conditions, frequency responses and transient responses for critical flight conditions are also presented in detail.

• KIISE Transactions on Computing Practices
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• v.20 no.10
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• pp.534-542
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• 2014

Multiscale modeling is a new simulation approach which can manage different spatial and temporal scales of system. In this study, as part of multiscale modeling research, we propose the way of combining two different simulation methods, molecular dynamics(MD) and stochastic rotation dynamics(SRD). Our conceptual implementations are based on LAMMPS, one of the well-known molecular dynamics programs. Our prototype of multiscale modeling follows the form of the third party implementation of LAMMPS. It added MD to SRD in order to simulate the boundary area of the simulation box. Because it is important to guarantee the seamless simulation, we also designed the overlap zones and communication zones. The preliminary experimental results showed that our proposed scheme is properly worked out and the execution time is also reduced.

• Aerospace Engineering and Technology
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• v.4 no.2
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• pp.15-20
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• 2005

Most of studies for the ground load and ground behavior of landing gear have been conducted with an assumption that the structure of landing gear was rigid body. The assumption of rigid body during design process results in many errors or discrepancy. High ground load occurs in 3 directions on the shock absorbing strut during landing. This ground load initiated high structural deformation. In this study, the flex-multi-body dynamics is applied to adapt flexible bodies, so the results of analysis can be described close to landing gears real behaviour.

• Proceeding of EDISON Challenge
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• 2015.03a
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• pp.201-206
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• 2015

이 논문에서는 역학적 지식파 EDISON 구조동역학 서버에서 지원하는 이공계 교육 및 연구용 시뮬레이션 프로그램 중 Co-rotational Plane Beam with Arbitrary Section을 이용하여 캔틸레버 보의 처짐을 기하 비선형적으로 해석한다. 또한 해석에 사용된 프로그램이 실제 교육에 적용이 가능한 지를 고찰함에 그 목적이 있다. 처짐을 해석하기 위하여 수계산, 프로그램을 이용하여 얻은 결과값을 비교하였고 캔틸레버 보의 변화 형상을 시각화 하였다.

• 기계와재료
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• v.23 no.4
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• pp.84-94
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• 2011

풍력발전기 동적 시뮬레이션 프로그램 개발을 위해 미국풍력기술연구센터(NWTC)의 프로그램군에 대해 분석하고 이를 소개하였다. 본 편에서 다물체 동역학 해석, 발전기, 제어 부분을 해석하는 FAST와 에어포일 데이터, 바람 데이터를 이용하여 공력을 계산하는 AeroDyn에 대해 설명하였고, 각 시간 단계마다 AeroDyn과 FAST 사이에 이루어지는 초기화 및 공력 전달 프로세스에 대해서도 소개하고자 한다.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.36 no.3
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• pp.339-346
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• 2012

The pre-evaluation of the current-collection performance is an important issue for high-speed railway vehicles. In this paper, using flexible multibody dynamic analysis techniques, a simulation model of the dynamic interaction between the catenary and pantograph is developed. In the analysis model, the pantograph is modeled as a rigid body, and the catenary wire is developed using the absolute nodal coordinate formulation, which can analyze large deformable parts effectively. Moreover, for the representation of the dynamic interaction between these parts, their relative motions are constrained by a sliding joint. Using this analysis model, the contact force and loss of contact can be calculated for a given vehicle speed. The results are evaluated by EN 50318, which is the international standard with regard to analysis model validation. This analysis model may contribute to the evaluation of high-speed railway vehicles that are under development.

• Proceedings of the Korean Society For Composite Materials Conference
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• 2001.10a
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• pp.206-209
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• 2001

This paper contains the development procedure of small-scaled composite rotor blade for helicopter hingeless rotor system. Composite blade design is conducted by using CORDAS program developed by KARI and dynamic analysis is conducted by using Flightlab which is commercial software for helicopter analysis. Also the optimizing procedure of iterative design was described. The designed composite blades were manufactured after establishing the effective curing method. Through this research, the experiences of composite rotor blade development were accumulated and will be applied to the related research field.