• 제목/요약/키워드: quasi static analysis

검색결과 411건 처리시간 0.023초

FPSO 다점 계류 시스템의 최적 설계 연구 (Study on Optimum Design of FPSO Spread Mooring System)

  • 임유창;김경수;정준모;김재우;김진태;여승훈
    • 한국해양공학회지
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    • 제23권6호
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    • pp.61-66
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    • 2009
  • For a spread-moored FPSO (Floating Production, Storage, & Off-loading) subjected to environmental excitation from waves, current, and wind, a procedure to determine optimum length and stiffness of mooring lines is suggested using quasi-static frequency domain response analyses. Coupled relations between design parameters are closely examined. In consideration of this, optimized design parameters are proposed based on minimum weight condition. The initial design parameters for numerical analyses are calculated using the static catenary equation of mooring lines. It is demonstrated the line tension and vessel's offset are influenced by the mooring line length and stiffness. Accordingly it is suggested the optimum vessel's offset range should be determined considering line fatigue damage. The availability and limitation of the application of quasi-static analysis method for spread mooring system are explained by comparing the result of time domain analysis with one of frequency domain analysis.

MPV 프레임의 피로수명 예측 (Fatigue Life Prediction of a Multi-Purpose Vehicle Frame)

  • 천인범;조규종
    • 한국자동차공학회논문집
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    • 제6권5호
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    • pp.146-152
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    • 1998
  • Recently, for the development of vehicle structures and components there is a tendency to increase using numerical simulation methods compared with practical tests for the estimation of the fatigue strength. In this study, an integrated powerful methodology is suggested for fatigue strength evaluation through development of the interface program to integrate dynamic analysis quasi-static stress analysis and fatigue analysis, which were so far used independently. To verify the presented evaluation method, a single and zigzag bump run test, 4-post road load simulation and driving durability test have been performed. The prediction results show a good agreement between analysis and test. This research indicates that the integrated life prediction methodology can be used as a reliable design tool in the pre-prototype and prototype development stage, to reduce the expense and time of design iteration.

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프레임 구조물에 대한 선형 내구 보강 기법의 적용 (Application of the Durability Reinforcement Technique on the Frame Structure)

  • 권성훈;유홍희
    • 대한기계학회논문집A
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    • 제33권11호
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    • pp.1341-1346
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    • 2009
  • In this paper, the technique to reinforce the durability performance of structure using the sensitivity information for the frame structure is applied. The fatigue life calculation for the frame structure is performed from the quasi-static and transient analysis and the characteristics of two methods are compared for the fatigue analysis. Then the reinforcement technique is applied. First, some design variables related to the locations of fatigue failure is selected. Then sensitivities of fatigue life at fracture points with respect to the variation of design variables are calculated and the vector composed of gaps between the target life and initial life cycles is calculated. If the number of fatigue fracture points is same as the number of design variables, the variations of the design variables are calculated from the linear algebraic equation. If not, the variations of the design variables are calculated from the optimization formulation with the constraints.

Ratcheting analysis of joined conical cylindrical shells

  • Singh, Jaskaran;Patel, B.P.
    • Structural Engineering and Mechanics
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    • 제55권5호
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    • pp.913-929
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    • 2015
  • The ratcheting and strain cyclic behaviour of joined conical-cylindrical shells under uniaxial strain controlled, uniaxial and multiaxial stress controlled cyclic loading are investigated in the paper. The elasto-plastic deformation of the structure is simulated using Chaboche non-linear kinematic hardening model in finite element package ANSYS 13.0. The stress-strain response near the joint of conical and cylindrical shell portions is discussed in detail. The effects of strain amplitude, mean stress, stress amplitude and temperature on ratcheting are investigated. Under strain symmetric cycling, the stress amplitude increases with the increase in imposed strain amplitude. Under imposed uniaxial/multiaxial stress cycling, ratcheting strain increases with the increasing mean/amplitude values of stress and temperature. The abrupt change in geometry at the joint results in local plastic deformation inducing large strain variations in the vicinity of the joint. The forcing frequency corresponding to peak axial ratcheting strain amplitude is significantly smaller than the frequency of first linear elastic axial vibration mode. The strains predicted from quasi static analysis are significantly smaller as compared to the peak strains from dynamic analysis.

매 시간단계의 등가정하중을 다중하중조건으로 이용한 준정적 구조최적화 방법 (Quasi-Static Structural Optimization Technique Using Equivalent Static Loads Calculated at Every Time Step as a Multiple Loading Condition)

  • 최우석;박경진
    • 대한기계학회논문집A
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    • 제24권10호
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    • pp.2568-2580
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    • 2000
  • This paper presents a quasi-static optimization technique for elastic structures under dynamic loads. An equivalent static load (ESL) set is defined as a static load set which generates the same displacement field as that from a dynamic load at a certain time. Multiple ESL sets calculated at every time step are employed to represent the various states of the structure under the dynamic load. They can cover every critical state that might happen at an arbitrary time. Continuous characteristics of dynamic load are simulated by multiple discontinuous ones of static loads. The calculated sets of ESLs are applied as a multiple loading condition in the optimization process. A design cycle is defined as a circulated process between an analysis domain and a design domain. Design cycles are repeated until a design converges. The analysis domain gives a loading condition necessary for the design domain. The design domain gives a new updated design to be verified by the analysis domain in the next design cycle. This iterative process is quite similar to that of the multidisciplinary optimization technique. Even though the global convergence cannot be guaranteed, the proposed technique makes it possible to optimize the structures under dynamic loads. It has also applicability, flexibility, and reliability.

압광 재료를 이용한 구조용 Y-TZP 소재의 고속 파괴현상 가시화 연구 (Visualization of High Speed fracture Behavior in Y-TZP by using Mechano-luminescence)

  • 김지식;손기선
    • 소성∙가공
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    • 제16권5호통권95호
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    • pp.348-353
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    • 2007
  • The propagation of a macro-scale crack and the accompanying transformation zone around it was visualized in an Y-TZP ceramic using a mechano-luminescence (ML) technique. The technique allows realistic fractures that take place catastrophically in actual applications to be realistically stimulated. Unlike conventional quasi-static R-curves, the ML technique on a relatively fast time frame permitted a so-called quasi-dynamic R-curve in the crack speed range from 50 to 140 m/sec. to be measured. Effective toughening then commenced and the applied stress intensity factor increased to 27 $MPa{\sqrt{m}}$. The transformation zone height obtained from the ML observations was in good agreement with that predicted by the Marshall model, and coincided with previously observed results for quasi-static conditions by Raman spectorscopy and x-ray analysis.

Static stability analysis of smart nonlocal thermo-piezo-magnetic plates via a quasi-3D formulation

  • Fenjan, Raad M.;Ahmed, Ridha A.;Faleh, Nadhim M.;Hani, Fatima Masood
    • Smart Structures and Systems
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    • 제26권1호
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    • pp.77-87
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    • 2020
  • By employing a quasi-3D plate formulation, the present research studies static stability of magneto-electro-thermo-elastic functional grading (METE-FG) nano-sized plates. Accordingly, influences of shear deformations as well as thickness stretching have been incorporated. The gradation of piezo-magnetic and elastic properties of the nano-sized plate have been described based on power-law functions. The size-dependent formulation for the nano-sized plate is provided in the context of nonlocal elasticity theory. The governing equations are established with the usage of Hamilton's rule and then analytically solved for diverse magnetic-electric intensities. Obtained findings demonstrate that buckling behavior of considered nanoplate relies on the variation of material exponent, electro-magnetic field, nonlocal coefficient and boundary conditions.

IMO Type B 탱크 상부 Rolling Chock에 대한 시간영역 피로해석 (Time Domain Fatigue Analysis on the Upper Rolling Chock of IMO Type B Tank)

  • 박명진;박준석;원선일;최병기;박경원;백영민;김유일
    • 대한조선학회논문집
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    • 제53권5호
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    • pp.380-387
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    • 2016
  • Present research target to develop the procedure of long-term fatigue analysis of the structural details near the upper rolling chock of IMO type B tank by using the time domain modal analysis technique where both the contact and friction behavior can be accurately simulated. In order to perform the time domain analysis focused on the contact and friction, the entire model of the hull and tank was condensed with DOF reduction technique, which is obtained by transforming the global finite element model into its quasi-static modal coordinate. Modal analysis using the quasi-static deformation modes is chosen as a cost effective time domain simulation method and this is based on the fact that the structural response of the tank is quasi-static. Based on the developed cost effective time domain simulation method, the long-term fatigue analysis procedure for the structural details near the rolling chock and key of independent type tank is targeted to be established. The developed fatigue assessment procedure takes into account, wave induced stress and both contact and friction induced stress without loss of accuracy.

연성하중해석을 통한 위성구조체의 구조안정성 검증 연구 (A Study on the Verifying Structural Safety of Satellite Structure by Coupled Load Analysis)

  • 김경원;김선원;임재혁;김창호;황도순
    • 한국위성정보통신학회논문지
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    • 제5권1호
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    • pp.63-68
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    • 2010
  • 인공위성 구조체는 발사환경과 궤도환경하에서 탑재체 및 여러 구동기 등을 안전하게 지지할 수 있도록 설계되어야 한다. 위성체의 형상설계가 이루어지면 상세설계를 위하여 발사체에서 공급하는 규격에 의한 준정적하중을 사용하여 구조해석을 수행한다. 이 때 준정적하중을 이용하여 설계된 위성체의 구조 건정성을 확인하기 위하여 발사체 업체는 위성체와 발사체를 연성한 후 연성하중해석을 수행한다. 현재 개발중인 위성체의 경우, 연성하중해석을 수행하기 위하여 위성체 모델을 Craig-Bampton 모델로 축약한 후, 발사체 제작업체로 전달하였다. 발사체 제작업체에서는 위성체 모델과 발사체 모델을 이용하여 연성하중해석을 수행하였으며, 가속도 결과와 변위결과를 계산하여 이를 전달하였다. 전달받은 가속도 결과와 변위결과로부터 위성체는 안전하게 설계되었으며, 위성체 내/외부에서 간섭이나 충돌의 위험성이 없다는 것을 확인하였다.

다층구조에서 도체 두께를 고려한 비대칭 결합선로의 특성해석 (Characteristic Analysis of the Asymmetric Coupled microstrip Lines with finite Metalization Thickness in the Multilayered Structure)

  • 윤남일;홍익표;박한규
    • 한국통신학회논문지
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    • 제25권3A호
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    • pp.424-429
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    • 2000
  • 본 논문에서는 준정적 해석방법을 사용하여 다층 구조에서 유한한 도체 두께를 갖는 비대칭결합 마이크로스트립(ACM: Asymmetric Couple Microstrip) 선로의 특성을 연구하였다. 준정적 해석방법으로서 모드정합법을 이용하였으며, ACM 선로의 특성 임피던스와 유효 유전율 상수가 도체 두께의 함수로 나타나는 결과를 얻었다. 수치해석 결과를 통해서 단층 및 다층구조에서 도체 두께의 변화로 인하여 ACM 선로의 전파특성이 변화되는 것으로 나타났다.

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