• Title/Summary/Keyword: 유한요소 해석코드

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Design Sensitivity Analysis for the Vibration Characteristics of Vehicle Structure (수송체 구조물의 진동특성에 관한 설계민감도 해석)

  • 이재환
    • Computational Structural Engineering
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    • v.7 no.1
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    • pp.91-98
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    • 1994
  • Design sensitivity analysis method for the vibration of vehicle structure is developed using adjoint variable method. A variational approach with complex response method is used to derive sensitivity expression. To evaluate sensitivity, FEM analysis of ship deck and vehicle structure are performed using MSC/NASTRAN installed in the super computer CRAY2S, and sensitivity computation is performed by PC. The accuracy of sensitivity is verified by the results of finite difference method. When compared to structural analysis time on CRAY2S, sensitivity computation is remarkably economical. The sensitivity of vehicle frame can be used to reduce the vibration responses such as displacement and acceleration of vehicle.

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Incompressible Laminar Entry Flows in a Square Duct of Strong Curvature Using an Implicit SMAC Scheme (SMAC 음해법에 의한 큰 곡률를 갖는 정사각형 덕트내의 비압축성 층류 입구유동)

  • Shin B. R.;Ikohagi T.
    • Journal of computational fluids engineering
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    • v.1 no.1
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    • pp.35-46
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    • 1996
  • 원심형 임펠러 내부 유로등 큰 곡률을 수반하는 터보기계 요소의 유동해석을 위한 계산코드를 개발하였다. 이 코드에서는 곡선좌표계에 유도된 3차원 비압축성 Navier-Stokes의 운동 방정식을 SMAC 음해법으로 푼다. 이 코드를 이용하여 유로의 단면이 정사각형이고 90도로 굽은 덕트내부의 층류 입구유동을 해석하고, 굽은 관 특유의 유동현상을 수치모사하였다 또한 곡관부 입구에서 충분히 발달한 유동, 또는 발달중인 유동이 유입될 경우에 이것이 곡관부 내부의 유동에 미치는 영향을 상·하류의 계산영역이 서로 다를 몇몇 유동장에 대하여 조사하고, 본 계산에서 얻어진 결과와 실형결과와의 비교로 본 3차원 유동해석 코드의 유효성을 검토 하였다.

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Design Considerations on Large-scale Parallel Finite Element Code in Shared Memory Architecture with Multi-Core CPU (멀티코어 CPU를 갖는 공유 메모리 구조의 대규모 병렬 유한요소 코드에 대한 설계 고려 사항)

  • Cho, Jeong-Rae;Cho, Keunhee
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.30 no.2
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    • pp.127-135
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    • 2017
  • The computing environment has changed rapidly to enable large-scale finite element models to be analyzed at the PC or workstation level, such as multi-core CPU, optimal math kernel library implementing BLAS and LAPACK, and popularization of direct sparse solvers. In this paper, the design considerations on a parallel finite element code for shared memory based multi-core CPU system are proposed; (1) the use of optimized numerical libraries, (2) the use of latest direct sparse solvers, (3) parallelism using OpenMP for computing element stiffness matrices, and (4) assembly techniques using triplets, which is a type of sparse matrix storage. In addition, the parallelization effect is examined on the time-consuming works through a large scale finite element model.

KALIMER 원자로구조물의 면진성능 및 내진여유도 평가

  • Yoo, Bong;Koo, Kyung-Hoe;Lee, Jae-Han
    • Proceedings of the Korean Nuclear Society Conference
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    • 1996.11b
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    • pp.683-689
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    • 1996
  • 본 논문의 목적은 현재 국내에서 개념설계중인 KALIMER(Korea Advanced LIquid MEtal Reactor) 원자로구조물에 대한 면진성능과 내진여유도를 평가하여 이들 성능을 향상시킬 수 있는 주요 설계변경 부위를 검토하는 것이다. 이를 위하여 ANSYS 범용 유한요소해석코드를 이용하여 원자로구조물에 대한 3차원 유한요소해석모델을 작성하고 이로부터 집중질량 스프링으로 이루어진 지진해석모델을 개발하여 지진해석을 수행하였다. KALIMER 원자로 구조물에 대한 내진평가결과 내진능력(Seismic Capability)은 0.35g로 나타났으며 이는 Reactor Vessel Liner, Separation Plate그리고 Support Barrel의 연결부위의 수직 강성을 증가시키는 설계변경을 통하여 크게 향상될 수 있는 것으로 나타났다.

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A Study of Flutter Analysis for the Composite Box Wings with Various Laminates (다양한 적층각에 대한 상자형 복합재료 날개의 플러터 특성연구)

  • Chung, Y.H.;Kwon, H.J.;Kim, D.H.;Lee, I.;Kim, C.G.
    • Composites Research
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    • v.15 no.1
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    • pp.1-8
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    • 2002
  • In this study, the flutter analysis for a rectangular box wing and an actual fighter wing with composite shin, aluminum spar and aluminum rib has been conducted. A conservative 3D wing-box model of an actual wing is modeled by MSC/PATRAN and the corresponding free vibration analysis has been performed by MSC/NASTRAN. The finite elements of membrane, rod and shear panel are used. Using the practical ply angles, various composite laminates are composed and analysed. The DLM code which is linear aerodynamic theory in frequency domain is applied to calculate unsteady aerodynamic pressure in subsonic flow region and the V-g and p-k methods are applied to obtain the solution of aeroelastic governing equation in frequency domain.

On the Explosive Welding Characteristics of Steel-Titanium Dissimilar Materials Using finite Element Method (유한요소법을 이용한 강-티타늄 이종소재의 폭발 용접조건 해석)

  • Kim, Chung-Kyun;Kim, Myung-Koo;Sim, Sang-Han;Moon, Jeong-Gi
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.20 no.3
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    • pp.825-831
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    • 1996
  • Using the two-dimensional hydrocode HI-DYNA2D, a calculation on the explosive selding of dissimilar plates(Steel Titanium) was made for the pressure, temperature, velocity and impact ingles adjacent to the collision point during the welding process. The FEM result indicates that optimal stand-off distance of initially parallel set-up is 3-5mm for various values of the explosive thickness. The calculation shows that when the explosive thickness is around 30mm, the temperature of welding point which is strongly related to the metallic jet formation is 2, 000-3, 500K for the given stand-off distance.

An Evaluation Method of Deformation Moduli using Finite Element Analysis of Cyclic Plate Load Tests (반복재하 평판재하시험의 유한요소해석을 이용한 변형계수의 추정기법)

  • Oh, Seboong;Seo, Wonseok;Kwon, Ohkyun
    • Journal of the Korean GEO-environmental Society
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    • v.8 no.6
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    • pp.61-68
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    • 2007
  • The problem on cyclic plate load tests was analyzed by finite element method using an anisotropic hardening constitutive model. The constitutive model was coded to user subroutine in ABAQUS. Using the result of the analysis, Young's moduli corresponding to various strain levels were evaluated by a back calculation method and were very similar to those of input. On the basis of the back calculation method plate loading tests were verified. As a result, deformation moduli could be evaluated practically from cyclic plate load tests with respect site conditions.

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MPI-OpenMP Hybrid Parallelization for Multibody Peridynamic Simulations (다물체 페리다이나믹 해석을 위한 MPI-OpenMP 혼합 병렬화)

  • Lee, Seungwoo;Ha, Youn Doh
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.33 no.3
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    • pp.171-178
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    • 2020
  • In this study, we develop MPI-OpenMP hybrid parallelization for multibody peridynamic simulations. Peridynamics is suitable for analyzing complicated dynamic fractures and various discontinuities. However, compared with a conventional finite element method, nonlocal interactions in peridynamics cost more time and memory. In multibody peridynamic analysis, the costs increase due to the additional interactions that occur when computing the nonlocal contact and ghost interlayer models between adjacent bodies. The costs become excessive when further refinement and smaller time steps are required in cases of high-velocity impact fracturing or similar instances. Thus, high computational efficiency and performance can be achieved by parallelization and optimization of multibody peridynamic simulations. The analytical code is developed using an Intel Fortran MPI compiler and OpenMP in NURION of the KISTI HPC center and parallelized through MPI-OpenMP hybrid parallelization. Further parallelization is conducted by hybridizing with OpenMP threads in each MPI process. We also try to minimize communication operations by model-based decomposition of MPI processes. The numerical results for the impact fracturing of multiple bodies show that the computing performance improves significantly with MPI-OpenMP hybrid parallelization.

Flow analysis of Ice Cone Die (아이스 콘 금형의 유동해석)

  • 이종선;김세환
    • Proceedings of the KAIS Fall Conference
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    • 2002.11a
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    • pp.253-257
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    • 2002
  • This study is object to flow analysis of ice cone die. The finite element model was developed to compute the flow, velocity and pressure for ice cone die. For flow analysis using result from FEM Code.