• Title/Summary/Keyword: 구조 동역학 모델

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Dynamic Characteristic Analysis by using Electric Circuit Parameter Extracted from Distributed Electromagnetic Systems (분포정수 전자기시스템에서 추출된 전기회로 상수를 이용한 동특성 해석)

  • Shin, Yu-Jeong;Han, Sang-Joon;Lee, Se-Hee;Park, Il-Han
    • Proceedings of the KIEE Conference
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    • 2002.11d
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    • pp.103-105
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    • 2002
  • 전기-기계 결합시스템에서의 동특성을 정확히 해석하기 위해서는 해석모델의 전기회로 방정식과 운동방정식이 함께 고려되어야 한다. 이때 시스템의 다양한 입력과 기하학적인 구조 등에 대한 등가회로 상수는 시스템의 전반적인 특성에 매우 민감하게 작용하므로 중요하게 고려 되어야한다. 본 논문에서는 전자기시스템의 회로상수를 미리 계산한 다음 이를 기계 역학시스템에 적용하여 다양한 전기적 입력과 외부 부하특성에 대하여 어떻게 동작하는지를 알아보았다. 전자기시스템의 회로상수 추출을 위해 전자장해석은 유한요소법을 이용하였으며 전기회로 방정식과 운동방정식이 함께 고려된 상태 미분방정식은 4차 Runge-Kutta 미분방정식 해법을 이용하여 운동특성을 해석하였다. 계산된 결과는 수학적으로 검증된 미분방정식과 비교하여 검증하였다.

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A Numerical Modeling of the East sea circulation (동해 순환의 수치모델)

  • Seung, Young-Ho;Kim, Kyun
    • 한국해양학회지
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    • v.28 no.4
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    • pp.292-304
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    • 1993
  • The east Sea circulation is numerically modeled with refined grid resolution elaborated open boundary condition, and by directly imposing the measured surface temperature and salinity typical the east Korean Warm current are clearer than those in previous works. among others, The Ulleung warm Water and the Intermediate Water of minimum salinity are nicely reproduced. The latter is formed in the northern/northwestern coastal region in winter and is advocated southward by strong under-current. the former is associated with a locally generated anti-cyclonic gyres. The model indicates strong seasonal variation of Nearshore Current along the Japanese coast from wintertime barotropic to summertime baroclinic structures. the associated strong reversed under-cur-rent in summer is not well understood. Global circulation pattern is characterized by two regions of cyclonic and anti-cyclonic gyres in the north and south, respectively. The presence of these gyres indicates importance of local dynamics in East Sea circulation. This model, however, does not completely resolve the problem of overshooting of the East Korean Warm current.

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The Separating Cover Using an Explosive Bolt and Spring Lever (폭발볼트 및 스프링 레버를 이용한 발사관 분리식 덮개)

  • Choi, Won-Hong;Shin, Sang-Mok
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.45 no.11
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    • pp.922-931
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    • 2017
  • This research paper describes design procedures and those verification with multi-body dynamic analysis and an experiment for the development of an unprecedented type of canister cover, named as the separating cover. In order to overcome drawbacks from the precious rupture type and actuator driven cover, the separating cover was suggested. It has the simplest structure composed of the previously developed explosive bolt and a spring-lever driven system. First of all, mechanical feasibility with proposed design parameters based on mathematical modeling was confirmed through dynamic analysis and then its results showed good agreement with the followed empirical results acquired from a high speed camera. On top of that, a parametric study was conducted to identify the effect of each design parameter on separating performance. It is highly expected that this research contributes to provide military industries with a brand new canister cover having simplicity and cost efficiency and thus it will be very useful in MLRS(Multiple Launch Rocket System).

Simulation of Stable Cloth on Triangular Mesh via LOD-Based Bending Springs on Strain-Based Dynamics

  • Jong-Hyun Kim
    • Journal of the Korea Society of Computer and Information
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    • v.28 no.9
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    • pp.73-79
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    • 2023
  • This paper describes a level of detail (LOD) based bending spring structure and damping technique that can reliably represent strain-based dynamics (SBD) on a triangular mesh. SBD models elastic energy using strain instead of energy based on the edge length of a triangular mesh. However, when a large external force occurs, the process of calculating the elastic energy based on edges results in a degenerate triangle, which stretches in the wrong direction because it calculates an unstable strain. In this paper, we introduce an LOD-based bending spring generation and energy calculation method that can efficiently handle this problem. As a result, the technique proposed in this paper can reliably and efficiently handle SBD based on bending springs, which can provide a stable representation of cloth simulation.

Study on the Levitation Stability of Maglev Vehicle considering the Vibration of Steel Switch Track (강재 분기기의 진동을 고려한 자기부상열차 부상안정성 연구)

  • Han, Jong-Boo;Park, Jinwoo;Han, Hyung-Suk;Lee, Jong-Min;Kim, Sung-Soo
    • Journal of the Korean Society for Railway
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    • v.18 no.3
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    • pp.175-185
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    • 2015
  • Generally, in the train area, switch tracks have required high reliability because this system is directly associated with derailment. Especially, switch tracks of Maglev vehicles must be moved in terms of the whole geometric characteristics, in which the bogies are encased in the switch track. For this reason, switch track was constructed with steel lighter than concrete girders. But, the steel switch track was weak because of structural vibration as well as structural deformation. Therefore, it is important to predict the levitation stability when a vehicle passes over flexible switch track. The aims of this paper are to develop a coupled dynamic model to describe the relationship between a Maglev vehicle and switch track and to predict the levitation stability. In order to develop the coupled dynamic model, a three dimensional vehicle model was developed based on multibody dynamics; a switch model was made using the modal superposition method. And, the developed model was verified using comparison measured data.

Aeroelastic Response Analysis for Wing-Body Configuration Considering Shockwave and Flow Viscous Effects (충격파 및 유동점성 효과를 고려한 항공기 날개-동체 형상에 대한 공탄성 응답)

  • Kim, Dong-Hyun;Kim, Yu-Sung;Hwang, Mi-Hyun;Kim, Su-Hyun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.37 no.10
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    • pp.984-991
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    • 2009
  • In this study, transonic aeroelastic response analyses have been conducted for the DLR-F4(wing-body) aircraft configuration considering shockwave and flow separation effects. The developed fluid-structure coupled analysis system is applied for aeroelastic computations combining computational structural dynamics(CSD), finite element method(FEM) and computational fluid dynamics(CFD) in the time domain. It can give very accurate and useful engineering data on the structural dynamic design of advanced flight vehicles. For the nonlinear unsteady aerodynamics in high transonic flow region, Navier-Stokes equations using the structured grid system have been applied to wing-body configurations. In transonic flight region, the characteristics of static and dynamic aeroelastic responses have been investigated for a typical wing-body configuration model. Also, it is typically shown that the current computation approach can yield realistic and practical results for aircraft design and test engineers.

Flow-Induced Vibration (FIV) Analysis of a 3D Axial Compressor Blade (3차원 축류압축기 블레이드의 유체유발진동 해석)

  • Kim, Dong-Hyun;Kim, Yu-Sung;Yang, Guo Wei;Jung, Kyu-Kang;Kim, Kyung-Hee;Min, Dae-Gee
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2009.04a
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    • pp.652-653
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    • 2009
  • In this study, flow-induced vibration (FIV) analyses have been conducted for a 3D compressor blade model. Advanced computational analysis system based on computational fluid dynamics (CFD) and computational structural dynamics (CSD) has been developed in order to investigate detailed dynamic responses of designed compressor blades. Fluid domains are modeled using the computational grid system with local grid deforming and remeshing techniques. Reynolds-averaged Navier-Stokes equations with $\kappa-\varepsilon$ turbulence model are solved for unsteady flow problems of the rotating compressor model. A fully implicit time marching scheme based on the Newmark direct integration method is used for computing the coupled aeroelastic governing equations of the 3D compressor blade for fluid-structure interaction (FSI) problems. Detailed dynamic responses and instantaneous pressure contours on the blade surfaces considering flow-separation effects are presented to show the multi-physical phenomenon of the rotating compressor blade.

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Numerical Study of Effect of counter-pulsation on Hemodynamic Response in the ECLS (체외생명구조장치에서 역박동 방법이 혈류역학 응답에 미치는 영향에 대한 수치적 연구)

  • Kim, In-Su;Lim, Ki-Moo;Choi, Seoung-Wook;Jun, Hyung-Min;Shim, Eun-Bo
    • Proceedings of the KSME Conference
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    • 2008.11a
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    • pp.1660-1664
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    • 2008
  • Extra-corporeal Life Support System (ECLS) is the device used in emergency cases to substitute a extracorporeal circulation in open heart surgery, cardiac arrest or in acute cardiopulmonary failure. To obtain the effect of counter-pulsation on hemodynamic response in the ECLS quantitatively, we developed cardiovascular model which consists of 12 compartment model of heldt et al. and 3 compartment model of Schreiner et al. based on windkessel approximation. We compared coronary perfusion, arterial pulse pressure, cardiac output, and left ventricular pressure-volume diagram according to flow configuration such as counter-pulsation, copulsation, and continous flow. When counter-pulsation was applied, 5% higher coronary perfusion, 26% lower pulse pressure, and 2% higher cardiac output than copulsation condition were calculated. We conclude that counter-pulsation configuration in the ECLS is hemodynamically more stable than copulsation and influences the positive effect to recover ventricles.

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Flame Response Modeling for Lean Premixed Combustors Using CFD (CFD를 이용한 희박 예혼합 연소기에서의 연소 응답 모델링)

  • Kim, Daesik;Lee, Jeongwon
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.38 no.9
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    • pp.773-779
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    • 2014
  • A qualitative and quantitative analysis on flame dynamics is required to model combustion instability characteristics in gas turbine lean premixed combustors. The current paper shows the flame transfer function modeling results using CFD(Computational Fluid Dynamics) techniques for the flame dynamics study. It is generally known that flame shapes determine the basic characteristics of the flame transfer function. The comparisons of the modeled flame shapes with the measured ones were made using the optimized heat transfer conditions. Modeling results of the flame transfer function show the close behaviors to the measured data with a reasonable accuracy if the flame geometry can be exactly captured.

Flow-induced Vibration(FIV) Analysis of a 3D Axial Compressor Blade (3차원 축류압축기 블레이드의 유체유발진동 해석)

  • Kim, Dong-Hyun;Kim, Yu-Sung;Yang, Guo Wei;Jung, Kyu-Kang;Kim, Kyung-Hee;Min, Dae-Gee
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.19 no.6
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    • pp.551-559
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    • 2009
  • In this study, flow-induced vibration(FIV) analyses have been conducted for a 3D compressor blade model. Advanced computational analysis system based on computational fluid dynamics(CFD) and computational structural dynamics(CSD) has been developed in order to investigate detailed dynamic responses of designed compressor blades. Fluid domains are modeled using the computational grid system with local grid deforming and remeshing techniques. Reynolds-averaged Navier-Stokes equations with $\kappa-\epsilon$ turbulence model are solved for unsteady flow problems of the rotating compressor model. A fully implicit time marching scheme based on the Newmark direct integration method is used for computing the coupled aeroelastic governing equations of the 3D compressor blade for fluid-structure interaction(FSI) problems. Detailed dynamic responses and instantaneous pressure contours on the blade surfaces considering flow-separation effects are presented to show the multi-physical phenomenon of the rotating compressor blade.