• 제목/요약/키워드: User subroutine

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통합형 점소성구성식을 이용한 손상재료거동해석 (Analysis of Damaged Material Response Using Unified Viscoplastic Constitutive Equations)

  • 하상렬;김기태
    • 대한기계학회논문집A
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    • 제29권2호
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    • pp.253-261
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    • 2005
  • In decades, a substantial body of work on a unified viscoplastic model which considers the mechanism of plastic deformation and creep deformation has developed. The systematic scheme for numerical analysis of unified model is necessary because the dominant failure mechanism is the defect growth and coalescence in materials. In the present study, the unified viscoplastic model for materials with defects suggested by Suquet and Michel was employed for numerical analysis. The constitutive equations are integrated based on the generalized mid-point rule and implemented into a finite element program (ABAQUS) by means of user-defined subroutine (UMAT). To evaluate the validity of the developed UMAT code and the assessment of the adopted viscoplastic model, the results obtained from the UMAT code was compared with the numerical reference solution and experimental data. The unit cell analysis also has been investigated to study the effect of strain rate, temperature, stress triaxiality and initial defect volume fraction on the growth and coalescence of the defect.

낙하체 충돌을 고려한 심해저 매니폴드 보호 구조물 설계 (Design of Subsea Manifold Protective Structure against Dropped Object Impacts)

  • 우선홍;이강수;정준모
    • 한국해양공학회지
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    • 제31권3호
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    • pp.233-240
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    • 2017
  • Subsea structures are always vulnerable to accidental risks induced by fishing gear, dropped objects, etc. This paper presents the design of a subsea manifold protective structure that protects against dropped object impacts. Probable dropped object scenarios were established considering the shapes and masses of the dropped objects. A design layout for the manifold protective structure was proposed, with detailed scantlings and material specifications. A method applicable to the pipelines specified in DNV-RP-F107(DNV, 2010) was applied to calculate the annual probabilities of dropped objects hitting the subsea manifold. Nonlinear finite element analyses provided the structural consequences due to the dropped object impacts such as the maximum deflections of the protective structure and the local fracture occurrences. A user-subroutine to implement the three-dimensional fracture strain surface was used to determine whether local fractures occur. The proposed protective structure was shown to withstand the dropped object impact loads in terms of the maximum deflections, even though local fractures could induce accelerated corrosion.

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

  • 오세붕;서원석;권오균
    • 한국지반환경공학회 논문집
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    • 제8권6호
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    • pp.61-68
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    • 2007
  • 본 연구에서는 비등방경화 구성모델을 이용하여 반복재하 평판재하시험에 대한 유한요소해석을 수행하였다. 이 때 구성모델은 ABAQUS 코드에서 제공하는 사용자 서브루틴에 적용하였다. 평판재하시험의 해석결과를 이용하여 영계수와 변형률을 역계산 하였으며 입력된 변형계수와 비교한 결과 적절하게 계산할 수 있는 것으로 판단되었다. 이러한 기법을 토대로 평판재하시험 사례에 대한 적용을 수행하였다. 이로부터 변형률에 따른 변형계수의 변화를 반복재하 평판재하시험 결과로부터 실용적으로 획득하는 것이 가능하였다.

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Comparison of steady and unsteady simulation methodologies for predicting no-load speed in Francis turbines

  • Hosseinimanesh, Hossein;Devals, Christophe;Nennemann, Bernd;Guibault, Francois
    • International Journal of Fluid Machinery and Systems
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    • 제8권3호
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    • pp.155-168
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    • 2015
  • No-load speed is an important performance factor for the safe operation of hydropower systems. In turbine design, the manufacturers must conduct several model tests to calculate the accurate value of no-load speed for the complete range of operating conditions, which are expensive and time-consuming. The present study presents steady and unsteady methods for calculating no-load speed of a Francis turbine. The steady simulations are implemented using a commercial flow solver and an iterative algorithm that relies on a smooth relation between turbine torque and speed factor. The unsteady method uses unsteady RANS simulations that have been integrated with a user subroutine to compute and return the value of runner speed, time step and friction torque. The main goal of this research is to evaluate and compare the two methods by calculating turbine dynamic parameters for three test cases consisting of high and medium head Francis turbines. Overall, the numerical results agreed well with experimental data. The unsteady method provided more accurate results in the opening angle range from 20 to 26 degrees. Nevertheless, the steady results showed more consistency than unsteady results for the three different test cases at different operating conditions.

얇은 막재료의 주름해석 기법 (Analysis Methods of Wrinkle Prediction for Thin Membrane)

  • 배홍수;우경식
    • 한국항공우주학회지
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    • 제41권11호
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    • pp.865-873
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    • 2013
  • 본 논문에서는 유한요소해석에 의한 막재료의 주름 해석 기법에 관하여 연구하였다. 삼각형 세일 형상에 대해 멤브레인 요소와 쉘 요소를 사용하여 주름해석을 수행하였다. 멤브레인 요소를 이용한 기법에서는 주름을 벌칙매개변수에 의한 물성치를 수정하는 알고리즘을 상용프로그램 내 사용자 서브루틴을 통하여 구현하였다. 쉘 요소에 의한 기하학적 비선형 후좌굴 기법에서는 면외방향의 좌굴을 발생시키기 위하여 모델의 메쉬에 작은 크기의 기하학적 결함을 심는 방법을 사용하였다. 쉘 방법에서는 내연 및 외연해석 기법을 고려하였다. 요소수의 증가에 따른 수렴성과 결과의 정확도의 관점에서 멤브레인 요소법과 쉘 요소법의 효율성을 비교하였다.

엔진 블리스크 제조를 위한 초내열합금 이종재의 HIP Diffusion Bonding (HIP Diffusion Bonding of Two Types of Superalloys for Engine Blisk Applications)

  • 나영상;황형철;염종택;권영삼;박노광
    • 소성∙가공
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    • 제12권1호
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    • pp.60-65
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    • 2003
  • HIP diffusion bonding of Ni-based superalloys, cast Mar-M247 (MM247) and Udimet 720 (U720) powder, was experimentally and numerically studied. Subsolvus HIP treatment was optimized by investigating the variations of high temperature tensile properties of HIP-bonded specimens with powder size, HIP'ing time, etc. While the tensile strength at high temperatures showed no detectable changes, the tensile elongation and reduction in area were slightly increased as the powder size decreased from -140 mesh to -270 mesh. While as-HIP'ed U720 showed a high tensile strength comparable to that of lorded U720 alloy, the HIP diffusion-bonded specimen showed a strength lower than the forged U720 alloy and the cast MM247 alloy The increase of HIP'ing tune from 2 hours to 3 hours resulted in a rapid risc of tensile strength and elongation due to the disappearence of microvoids in the cast MM247. FEM simulation for HIP process was conducted by applying the McMeeking micromechanical model, which uses power-law creep model as constitutive equations. ABAQUS user subroutine CREEP with an implemented microscopic model was used for the simulation. Numerical simulation was shown to be essential for the near-net shape manufacturing as well as the HIP process optimization.

Punching Fracture Experiments and Simulations of Unstiffened and Stiffened Panels for Ships and Offshore Structures

  • Park, Sung-Ju;Choung, Joonmo
    • 한국해양공학회지
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    • 제34권3호
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    • pp.155-166
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    • 2020
  • Ductile fracture prediction is critical for the reasonable damage extent assessment of ships and offshore structures subjected to accidental loads, such as ship collisions and groundings. A fracture model combining the Hosford-Coulomb ductile fracture model with the domain of solid-to-shell equivalence model (HC-SDDE), was used in fracture simulations based on shell elements for the punching fracture experiments of unstiffened and stiffened panels. The flow stress and ductile fracture characteristics of JIS G3131 SPHC steel were identified through tension tests for flat bar, notched tension bar, central hole tension bar, plane strain tension bar, and pure shear bar specimens. Punching fracture tests for unstiffened and stiffened panels are conducted to validate the presented HC-DSSE model. The calibrated fracture model is implemented in a user-defined material subroutine. The force-indentation curves and final damage extents obtained from the simulations are compared with experimental results. The HC-DSSE fracture model provides reasonable estimations in terms of force-indentation paths and residual damage extents.

변온 하중하에 있는 재료의 이력거동 예측을 위한 다층 모델에 관한 연구 (A Study on the Overlay Model for Description of Hysteresis Behavior of a Material under Non-isothermal Loading)

  • 김상호;서동훈;여태인
    • 한국자동차공학회논문집
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    • 제18권3호
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    • pp.133-142
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    • 2010
  • The present work focuses on the characterization of material parameters of the Overlay(multilinear hardening) model for analyzing the non-isothermal cyclic deformation. In the previous study, all the parameters were especially based on the Overlay theories, and a simple method was suggested to find out the best material parameters for the isothermal cyclic deformation analysis. Based on the previous research this paper f dther improves the isothermal parameters and suggests how to apply the isothermal parameters to the non-isothermal conditions especially for the description of TMF(Thermo-Mechanical Fatigue) hysteresis behavior. The parameters are determined and calibrated using 400 series stainless steel test data in the reference papers. For the implementation into ABAQUS, a user subroutine is developed by means of ABAQUS/UMAT. The finite element results show good agreement with test for the case of uniaxial non-isothermal cyclic loading, signifying the proposed method can be used in the TMF analysis of the converter-inserted heavy duty muffler system and the stainless steel exhaust-manifold system which are to be done in our future research.

점소성 모델을 이용한 액체로켓 연소기 재생냉각 채널 구조해석 (Structural analysis of liquid rocket thrust chamber regenerative cooling channel using visco-plastic model)

  • 류철성;최환석
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2006년도 제26회 춘계학술대회논문집
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    • pp.151-155
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    • 2006
  • Bodner-Partom 점소성 모델을 이용하여 액체로켓 연소기 재생냉각 챔버의 구조해석을 수행하였다. 구조해석에 사용한 점소성 모델의 재료상수를 구하기 위하여 구리합금에 대하여 변형률 속도를 변화시켜 인장시험을 상온 및 고온에서 수행하였다. 점소성 모델의 재료상수는 구리합금의 변형률 속도 시험 데이터로부터 구하여 사용하였으며 점소성 모델의 구현은 상용유한요소 해석 프로그램인 Marc의 사용자 서브루틴을 이용하여 구현하였다. 구조해석 결과 냉각 채널은 압력에 의한 영향보다 열하중에 의하여 대부분의 변형이 발생하며 연소기의 작동조건에서 냉각 채널의 안정성 여부를 확인할 수 있었다.

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Bodner-Partom 점소성 모델을 이용한 액체로켓 연소기 재생냉각 채널 구조해석 (Structural Analysis of Liquid Rocket Thrust Chamber Regenerative Cooling Channel using Bodner-Partom Viscoplastic Model)

  • 류철성;백운봉;최환석
    • 한국추진공학회지
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    • 제10권4호
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    • pp.69-76
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    • 2006
  • Bodner-Partom 점소성 모델을 이용하여 액체로켓 연소기 재생냉각 챔버의 구조해석을 수행하였다. 구조해석에 사용한 점소성 모델의 재료상수를 구하기 위하여 구리합금에 대하여 변형률 속도를 변화시켜 인장시험을 상온 및 고온에서 수행하였다. 점소성 모델은 상용유한요소 해석 프로그램인 Marc의 사용자 서브루틴을 이용하여 구현하였다. 구조해석 결과 냉각 채널은 압력에 의한 하중보다 열하중에 의하여 대부분의 변형이 발생하며 연소기의 작동조건에서 냉각 채널의 구조적인 안정성 여부를 확인할 수 있었다.