• Title/Summary/Keyword: Multi-body Dynamics Program

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Dynamic Analysis of Railway Vehicle Having Single Axle Bogie (1축 대차용 철도차량의 동특성 해석)

  • Yang, Hee-Joo;Oh, Taek-Yul
    • Journal of the Korean Society for Precision Engineering
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    • v.18 no.3
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    • pp.84-89
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    • 2001
  • Studied in this paper was the vehicle dynamics simulation for development of single axle bogie using the multi-body dynamics simulation program(VAMPIRE). Single axle bogie vehicle is to the crew of freight vehicle. Method of analysis for dynamic behaviors of vehicle having single axle bogie was carried by UIC(International Union of Railways) code 518 and results of analysis were presented in terms of the hunting stability and the derailment ratio and the sum of wheel/rail lateral force. The results of analysis meet the criteria proposed by UIC.

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Dynamic Behavior Analysis of the Auto-leveling System for Large Scale Transporter Type Platform Equipment on the Ground Slope (경사지에서 운용 가능한 대형 차량형 플랫폼 장비 자동수평조절장치의 동적 거동)

  • Ha, Taewan;Park, Jungsoo
    • Journal of the Korea Institute of Military Science and Technology
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    • v.23 no.5
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    • pp.502-515
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    • 2020
  • To identify the dynamic characteristics of the Auto-leveling system applied to the Tractor-Trailer type Transporter for mounting a large scale precision equipment, Dynamics Modeling & Simulation were performed using general Dynamics Analysis Program - RecurDyn(V9R2). The axial load data, transverse load data and pad trace data of leveling actuators were obtained from M&S. And they were analyzed and compared with each other by parameters, i.e. friction coefficients on the ground, landing ram speed of actuators, and direction & quantity of ground slope. It was observed that ground contact friction coefficients affected to transverse load and pad trace; the landing ram speed of actuators to both amplitude of axial & transverse load, and this phenomena was able to explain from the frequency analysis of the axial load data; the direction of ground slope to driving sequence of landing ram of actuators. But the dynamic behaviors on the two-directional slope were very different from them on the one-directional slope and more complex.

Analysis of Dynamic Characteristics for Four-Wheel-Steering Automated Guided Vehicle(AGV) System (4륜 조향 무인 컨테이너 차량(AGV) 시스템의 동특성 분석)

  • 최재영;이영진;변성태;이권순;이만형
    • 제어로봇시스템학회:학술대회논문집
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    • 2000.10a
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    • pp.306-306
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    • 2000
  • This paper analyze the dynamic characteristics of Automated Guided Vehicle(AGV) which is being developed as a part of automation in port through DADS, one of the multi-dynamic analysis program, Previous evaluation of a vehicle is carried out through the continuous driving test of a real vehicle, however this method raise the loss of finance and time. If it is possible to analyze the dynamic characteristics of vehicle before construction completely we can compensate the loss of money and time during constructing. AGV contained containers is very heavy and its center of gravity can be easily changed with the disturbance from road or cornering. It makes AGV unsatisfied, therefore we evaluate the handling characteristics and stability of the full vehicle model. This paper contribute to establish the foundation of the development of a new system like a AGV which have a special structure.

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Development of Aerodynamic Analysis Technology for Wind Turbines using a Multibody Dynamic Analysis Software (다물체 동력학 해석 프로그램을 이용한 풍력발전기 공력해석 기술개발)

  • Rim, Chae Whan;Bang, Je Sung;Cho, Huije;Moon, Seok Jun;Chung, Tae Young
    • 한국신재생에너지학회:학술대회논문집
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    • 2010.06a
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    • pp.180.2-180.2
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    • 2010
  • Simulation technology for dynamic analysis of wind turbine is developed. The Aerodyn and the DAFUL are chosen for aerodynamic analysis and multi-body and flexible body dynamics respectively. Subroutines and variables of Aerodyn developed by NREL are analyzed with hub-height wind data, full field turbulent wind data and Airfoil data. The interface to perform coupled analysis between AeroDyn and DAFUL, GUI for modeling several parts of wind turbines are developed. The program will be extended to analyze the coupled analysis of aerodynamic and hydrodynamic behavior for floating offshore wind turbines.

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Introduction to the NREL Design Codes for System Performance Test of Wind Turbines - Part II : Simulators (풍력터빈 시스템 성능평가를 위한 NREL 프로그램군에 관한 소개 - 해석기를 중심으로)

  • Bang, Je-Sung;Rim, Chae Whan;Chung, Tae Young
    • 한국신재생에너지학회:학술대회논문집
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    • 2011.11a
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    • pp.42.1-42.1
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    • 2011
  • NREL NWTC Deside codes are analyzed and introduced to develop the system performance simulation program for wind turbine generator systems. In this paper, The FAST performing multi-body and flexible body dynamics, control and the AeroDyn calculating aerodynamic forces with airfoil data and wind data are explained. Furthermore, initialization and process for transfer of aerodynamic force between AeroDyn and FAST at each time step are also introduced.

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TIDAL TAILS OF GLOBULAR CLUSTERS

  • YIM KI-JEONG;LEE HYUNG MOK
    • Journal of The Korean Astronomical Society
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    • v.35 no.2
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    • pp.75-85
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    • 2002
  • We present N-body simulations of globular clusters including gravitational field of the Galaxy, in order to study effects of tidal field systematically on the shape of outer parts of globular clusters using NBODY6. The Galaxy is assumed to be composed of central bulge and outer halo. We mvestigate the cluster of multi-mass models with a power-law initial mass function (IMF) starting with different initial masses, initial number of particles, different slopes of the IMF and different orbits of the cluster. We have examined the general evolution of the clusters, the shape of outer parts of the clusters, density profiles and the direction of tidal tails. The density profiles appear to become somewhat shallower just outside the tidal boundary consistent with some observed data. The position angle of the tidal tall depends on the location in the Galaxy as well as the direction of the motion of. clusters. We found that the clusters become more elongated at the apogalacticon than at the pengalacticon. The tidal tails may be used to trace the orbital paths of globular clusters.

Separation characteristics of particles in a self-rotating type centrifugal oil purifier

  • Pyo, Young-Seok;Jung, Ho-Yun;Choi, Yoon-Hwan;Doh, Deog-Hee;Lee, Yeon-Won
    • Journal of Advanced Marine Engineering and Technology
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    • v.38 no.2
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    • pp.147-153
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    • 2014
  • The centrifugal oil purifier is used in an engine for lubrication and to remove impurities. The momentum needed for the rotation of the cylindrical chamber is obtained by jet injections. An impure particle in the oil is separated by the centrifugal forces moving to the inner wall of the rotating cylindrical chamber body. The dust particles are eliminated when the particles are absorbed onto the surface of the inner wall of the chamber body. The flow characteristics and the physical behaviors of particles in this centrifugal oil purifier were investigated numerically and the filtration efficiencies was evaluated. For calculations, a commercial code is used and the SST (Shear Stress Transport) turbulence model has been adopted. The MFR (Multi Frames of Reference) method is introduced to consider the rotating effect of the flows. Under various variables, such as particle size, particle density and rotating speed, the filtration efficiencies are evaluated. It has been verified that the filtration efficiency is increased with the increments in the particle size, the particle density and the rotating speed of the cylindrical chamber.

Solar Array Deployment Analysis of a Satellite (인공위성 태양전지판 전개해석)

  • Kim, Kyung-Won;Kim, Sun-Won;Lim, Jae-Hyuk;Rhee, Ju-Hun;Hwang, Do-Soon;Jin, Ik-Min;Kim, Hak-Jung;Song, Woon-Hyung;Choi, Hang-Suk
    • Journal of Satellite, Information and Communications
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    • v.3 no.1
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    • pp.29-34
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    • 2008
  • After spacecraft is separated from the launch vehicle, first of all spacecraft deploy the solar array. Solar array deployment is one of the key factors deciding the success of the spacecraft mission. Therefore, It is necessary to predict the solar array deployment motion and check the safety through calculating the load on the tape hinges of solar array using the deployment analysis in the initial design phase. In this paper, solar array deployment analysis is performed by multi-body dynamics simulation program. From the analysis results, assessment on the safety also is carried out. In addition, hinge characteristic test is fulfilled to find out hinge characteristic, and is applied to the deployment analysis.

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Multi-body Dynamic Analysis for Tripod Constant Velocity Joint (트라이포드 타입 등속조인트의 다물체 동역학 해석)

  • Song, Myung-Eui;Lim, Young-Hun;Cho, Hui-Je;Bae, Dae-Sung
    • Transactions of the Korean Society of Automotive Engineers
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    • v.18 no.1
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    • pp.1-7
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    • 2010
  • The paper proposes a multi-body dynamic simulation to numerically evaluate the generated axial force(G.A.F) and plunging resistant force(P.R.F) practically related to the shudder and idling vibration of an automobile. A numerical analysis of two plunging types of CV joints, tripod joint(TJ) and very low axial tripod joint(VTJ), is conducted using the commercial program DAFUL. User-defined subroutines of a friction model illustrating the contacted parts of the outboard and inboard joint are subsequently developed to overcome the numerical instability and improve the solution performance. The Coulomb friction effect is applied to describe the contact models of the lubricated parts in the rolling and sliding mechanisms. The numerical results, in accordance with the joint articulation angle variation, are validated with experimentation. The offset between spider and tulip housing is demonstrated to be the critical role in producing the 3rd order component of the axial force that potentially causes the noise and vibration in vehicle. The VTJ shows an excellent behavior for the shudder when compared with TJ. In addition, a flexible nonlinear contact analysis coupled with rigid multi-body dynamics is also performed to show the dynamic strength characteristics of the rollers, housing, and spider.

Flight Dynamic Simulation Program for Analyzing Static and Dynamic Behaviors of Aircraft with Flexible Characteristics (유연 특성 항공기의 동적·정적 거동 분석을 위한 비행 동역학 시뮬레이션 프로그램)

  • Jin, Jaehyun;Paek, Seung-Kil
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.49 no.1
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    • pp.31-40
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    • 2021
  • Modern aircraft are high-performance and lightweight. Thus, the characteristics of the flexible structure appear and affect flight performance or limit it. These flexible characteristics need to be analyzed from the early stages of aircraft design. To this end, a program to analyze the dynamic and static behavior of flexible aircraft has been developed and the results are presented. Based on the multi-body dynamics simulation technique, rigid flight mechanics, structural vibrating behavior, and unsteady aerodynamics have been developed and integrated. Lastly, the level flight and the turn flight of the flexible characteristic aircraft have been analyzed using this integrated simulation program.