• Title/Summary/Keyword: Computational structure analysis

Search Result 1,634, Processing Time 0.028 seconds

ALE-Based FSI Simulation of Solid Propellant Rocket Interior (ALE 기반의 고체 로켓 내부 유체-구조 연계 해석)

  • Han, Sang-Ho;Choi, H.S.;Min, D.H.;Kim, C.;Hwang, Chan-Gyu
    • 한국전산유체공학회:학술대회논문집
    • /
    • 2008.03b
    • /
    • pp.510-513
    • /
    • 2008
  • The traditional computational fluid or structure dynamics analysis approaches have contributed to solve many delicate engineering problems. But for the most of recent engineering problems which are influenced by fluid-structure interaction effect strongly, traditional individual approaches have limited analysis abilities for the exact simulation. Owing to above-mentioned reason, nowadays fluid-structure interaction analysis has become a matter of concern and interest. FSI analysis require several unprecedented techniques for the combining individual analysis tool into integrated analysis tool. The Arbitrary Lagrangian-Eulerian(ALE, in short) method is the new description of continum motion,which combines the advantages of the classical kinematical descriptions, i.e. Lagrangian and Eulerian description, while minimizing their respective drawbacks. In this paper, the ALE description is adapted to simulate fluid-structure interaction problems. An automatic re-mesh algorithm and a fluid-structure coupling process are included to analyze the interaction and moving motion during the 2-D axisymmetric solid rocket interior FSI phenomena simulation.

  • PDF

Static Aeroelastic analysis of Morphing flap wign through FSI analysis method (FSI를 이용한 모핑 플랩 날개의 정적 공탄성 해석)

  • Kim, Jonghwan;Ko, Seughee;Bae, Jaesung;Hwang, Jaihyuk
    • Journal of Aerospace System Engineering
    • /
    • v.6 no.4
    • /
    • pp.1-6
    • /
    • 2012
  • The morphing flap wing has different structure unliked general wing structure. The actuated chord length of the morphing flap was more longer than conventional wing flap. In this reason, morphing flap wing structure was important to bending moment by aerodynamic lift force. In this study, through the fluid-structure interaction using computational fluid dynamics and structure finite element analysis to apply that the morphing flap wing's static aeroelastic stability analysis.

The Analytical Model Considering the Deformation of Panel Zone with Linear Element (선형요소를 사용하여 판넬존 변형을 고려한 해석 모텔)

  • 조소훈;박찬헌;이동근
    • Proceedings of the Computational Structural Engineering Institute Conference
    • /
    • 2004.04a
    • /
    • pp.293-300
    • /
    • 2004
  • As the structure is taller and its member is larger, the effect of the deformation of Panel zone on the displacement of structure becomes larger. The analysis using the centerline dimensions in the steel moment frame structure can not consider the accurate effect of panel ton And the finite element analysis using infinitesimal solid and shell element is impractical for the total tall building structure. Therefore, this paper proposes the analytical model using linear element in order to be able to evaluate the reasonable deformation of panel zone. the proposed analytical model makes the analysis of the building structure simple and ease because it uses the only linear elements. In addition it can easily incorporate the various parameters affecting the deformation of panel zone. In order to prove the validith of the prosed analytical model, the analysis result using the proposed analytical model is compared with the result using finite element analysis with shell element

  • PDF

Ship Collision Analysis with Offshore Structure (선박과 해양 구조물의 충돌 해석)

  • Kim, Jong-Sung;Jung, Hyun;Ko, Jae-Yong
    • Proceedings of the Computational Structural Engineering Institute Conference
    • /
    • 2004.04a
    • /
    • pp.169-176
    • /
    • 2004
  • Offshore structure crossing navigation waterways must not only be designed to resist gravity, wind, and earthquake load, but also be capable of resisting ship and barge collision load. Current specifications for offshore structure design provide empirical relationships for computing impact loads generated during barge collision, however, these relationships are based on the limited experimental data. In this paper, the dynamic finite element analysis is used to computing force for vessel collision scenarios to offshore structures. Results obtained from the ANSYS/LS-DYNA are compared to AASHTO bridge design specifications.

  • PDF

Fluid-structure-interacted Finite Element Analysis of Valve System In a Linear Compressor (선형압축기 밸브시스템의 유체-구조 연성 유한요소해석)

  • Choi, Yong-Sik;Lee, Jun-Ho;Jeong, Weui-Bong;Cheong, Cheol-Ung
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
    • /
    • 2008.11a
    • /
    • pp.121-122
    • /
    • 2008
  • In this paper, computational analysis on the steady-state and transient behaviors of the valve system is discussed. Fluid-structure interaction (FSI) is taken into account using ADINA software. The computational results are experimentally validated.

  • PDF

A Development of Data Structure and Mesh Generation Algorithm for Global Ship Analysis Modeling System (선박의 전선해석 모델링 시스템을 위한 자료구조와 요소생성 알고리즘 개발)

  • Kim I.I.;Choi J.H.;Jo H.J.;Suh H.W.
    • Korean Journal of Computational Design and Engineering
    • /
    • v.10 no.1
    • /
    • pp.61-69
    • /
    • 2005
  • In the global ship structure and vibration analysis, the FE(finite element) analysis model is required in the early design stage before the 3D CAD model is defined. And the analysis model generation process is a time-consuming job and takes much more time than the engineering work itself. In particular, ship structure has too many associated structural members such as stringers, stiffness and girders etc. These structural members should be satisfied as the constraints in analysis modeling. Therefore it is necessary to support generation of analysis model with satisfying these constraints as an automatic manner. For the effective support of the global ship analysis modeling, a method to generate analysis model using initial design information within ship design process, that hull form offset data and compartment data, is developed. In order to easily handle initial design information and FE model information, flexible data structure is proposed. An automatic quadrilateral mesh generation algorithm using initial design information to satisfy the constraints imposed on the ship structure is also proposed. The proposed data structure and mesh generation algorithm are applied for the various type of vessels for the usability test. Through this test, we have verified the stability and usefulness of this system including mesh generation algorithm.

Evaluation of Ultimate Pressure Capacity of Wolsong Containment Structure (월성 원자력발전소 격납건물의 극한내압평가)

  • Kwak Hyo-Gyoung;Kim Jae Hong;Kim Sun-Hoon;Chung Yun-Suk
    • Proceedings of the Computational Structural Engineering Institute Conference
    • /
    • 2005.04a
    • /
    • pp.183-189
    • /
    • 2005
  • Nuclear containment structure is the last barrier for being secure from any nuclear power plant accident. Even though the safety requirements of nuclear power plant have been focused on removing accidental situations, nuclear containment structure must reserve the sufficient resisting capacity to any accident because it works as the last barrier. The acceptable nuclear containment structure makes possible to limit the effect of internal accidents and to avoid radioactive release. In this study, to conduct the numerical analysis for the structural safety of a containment structure, loss of coolant accident (LOCA) is considered as the basic accidental load, and Wolsong containment structure is considered as a target structure. The CANDU containment structure, such as Wolsong containment structure, is a prestressed concrete shell structure which has dome and is reinforced with bonded tendons. The evaluation of ultimate pressure capacity was conducted by nonlinear analysis of a prestressed concrete containment structure.

  • PDF

Computational Flow Analysis on Improvement Effect of Wind Shear by a Structure Installed Upstream of a Wind Turbine (풍력발전기 풍상부 지면설치 구조물에 의한 풍속전단 개선효과의 전산유동해석)

  • Kim, Hyun-Goo;Woo, Sang-Woo;Jang, Moon-Seok;Shin, Hyuong-Ki
    • 한국신재생에너지학회:학술대회논문집
    • /
    • 2008.05a
    • /
    • pp.278-281
    • /
    • 2008
  • This study demonstrates the advantages of a shear-free structure designed to modify vertical profiles of wind speed in the atmospheric surface layer. Computational fluid dynamics(CFD) software, FLUENT is used to interpret the velocity field modification around the structure and wind turbine. The shapes of shear-free structure, installed at upstream toward prevailing wind direction, would be fences, buildings and trees, etc. According to the simulation results, it is obvious that wind shear between heights of wind turbine's blades is decreased together with a speed-up advantage. This would lead decrease of periodic wind loading caused by wind shear and power-out increase by flow uniformity and wind speed-up.

  • PDF

Comparative study on cracked beam with different types of cracks carrying moving mass

  • Jena, Shakti P.;Parhi, Dayal R.;Mishra, Devasis
    • Structural Engineering and Mechanics
    • /
    • v.56 no.5
    • /
    • pp.797-811
    • /
    • 2015
  • An analytical-computational method along with finite element analysis (FEA) has been employed to analyse the dynamic behaviour of deteriorated structures excited by time- varying mass. The present analysis is focused on the comparative study of a double cracked beam with inclined edge cracks and transverse open cracks subjected to traversing mass. The assumed computational method applied is the fourth order Runge-Kutta method. The analysis of the structure has been carried out at constant transit mass and speed. The response of the structure is determined at different crack depth and crack inclination angles. The influence of the parameters like crack depth and crack inclination angles are investigated on the dynamic behaviour of the structure. The results obtained from the assumed computational method are compared with those of the FEA for validation and found good agreements with FEA.

Soil-Structure Interaction Analysis Method in Time Domain considering Near-Field Nonlinearity (근역지반의 비선형성을 고려한 시간영역 지반-구조물 상호작용 해석기법의 개발)

  • 김문겸;임윤묵;김태욱;박정열
    • Proceedings of the Computational Structural Engineering Institute Conference
    • /
    • 2001.04a
    • /
    • pp.309-314
    • /
    • 2001
  • In this study, the nonlinear soil structure interaction analysis method based on finite element and boundary element method is developed. In the seismic region, the nonlinearity of near field soil has to be considered for more exact reflection of soil-structure interaction effect. Thus, nonlinear finite element program coupled with boundary elements is developed for nonlinear soil-structure interaction analysis. Using the developed numerical algorithm, the nonlinear soil-structure interaction analysis is performed and responses due to dynamic forces and seismic excitation are investigated. The developed method is verified by comparing with previous studies.

  • PDF