• 제목/요약/키워드: stress failure

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주조 알루미늄합금 A356의 저주기 피로특성 및 피로수명 모델 (Low Cycle Fatigue Characteristics of A356 Cast Aluminum Alloy and Fatigue Life Models)

  • 고승기
    • 한국자동차공학회논문집
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    • 제1권1호
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    • pp.131-139
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    • 1993
  • Low cycle fatigue characteristics of cast aluminum alloy A356 with a yield strength and ultimate strength of 229 and 283 MPa respectively was evaluated using smooth axial specimen under strain controlled condition. Reversals to failure ranged from 16 to 107. The cast aluminum alloy exhibited cyclically strain-gardening behavior. The results of low cycle fatigue tests indicated that the conventional low cycle fatigue tests indicated that the conventional low cycle fatigue life model was not a satisfactory representation of the data. This occurred because the elastic strain-life curve was not-log-log linear and this phenomena caused a nonconservative and unsafe fatigue life prediction at both extremes of long and short lives. A linear log-log total strain-life model and a bilinear log-log elastic strain-life model were proposed in order to improve the representation of data compared to the conventional low cycle fatigue life model. Both proposed fatigue life models were statistically analyzed using F tests and successfully satisfied. However, the low cycle fatigue life model generated by the bilinear log-log elastic strain-life equation yielded a discontinuous curve with nonconservatism in the region of discontinuity. Among the models examined, the linear log-log total strain-life model provided the best representation of the low cycle fatigue data. Low cycle fatigue life prediction method based on the local strain approach could conveniently incorporated both proposed fatigue life models.

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국부 안정성을 고려한 인공위성 모듈의 구조 최적설계 (Optimal Design of a Satellite Module Considering Local Stabilities)

  • 박정선;임종빈;김진희;진익민
    • 한국항공우주학회지
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    • 제31권8호
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    • pp.36-43
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    • 2003
  • 본 연구에서는 탑재체 장착을 위한 인공위성의 탑재부에 대한 모듈 단위 구조 최적설계를 수행하였다. 구조 최적화에 있어, 고유진동수 및 응력과 같은 일반적인 제한조건이외에 우주 발사환경에서 특별히 고려하는 링클링, 딤플링, 크림핑 응력과 같은 하니컴 부재의 불안정성 조건 및 론저론의 크리플링 파단을 추가로 고려하였다. 이러한 다양한 제한 조건을 포함하기 위해, 본 연구에서는 최적화프로그램과 구조해석프로그램을 연결하여 해석을 수행하였다. 해석 결과 탑재모듈의 최적화에 큰 영향을 미친 제한 조건은 고유진동수, 크리플링 그리고, 링클링 임을 알 수 있었다. 또한 설계변수들의 변화를 통해서 탑재모듈의 구조적인 특성에 가장 많은 영향을 주는 부재를 확인 할 수 있었다. 결론적으로, 탑재모듈의 특수한 제한조건을 고려한 최적화를 통해서 주어진 조건에 더 효율성 있고 안정성 있는 탑재모듈의 구조 최적화설계를 도출할 수 있었다.

Biomechanical stability of internal bone-level implant: Dependency on hex or non-hex structure

  • Lee, Hyeonjong;Park, Si-Myung;Noh, Kwantae;Ahn, Su-Jin;Shin, Sangkyun;Noh, Gunwoo
    • Structural Engineering and Mechanics
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    • 제74권4호
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    • pp.567-576
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    • 2020
  • Considerable controversy surrounds the choice of the best abutment type for implant prosthetics. The two most common structures are hex and non-hex abutments. The non-hex abutment typically furnishes a larger contact area between itself and the implant than that provided by a hex structure. However, when a hex abutment is loaded, the position of its contact area may be deeper than that of a non-hex abutment. Hence, the purpose of this study is to determine the different biomechanical behaviors of an internal bone-level implant based on the abutment type-hex or non-hex-and clinical crown length under static and cyclic loadings using finite element analysis (FEA). The hex structure was found to increase the implant and abutment stability more than the nonhex structure among several criteria. The use of the hex structure resulted in a smaller volume of bone tissues being at risk of hypertrophy and fatigue failure. It also reduced micromovement (separation) between the implant components, which is significantly related to the pumping effect and possible inflammation. Both static and fatigue analyses, used to examine short- and long-term stability, demonstrated the advantages of the hex abutment over the non-hex type for the stability of the implant components. Moreover, although its impact was not as significant as that of the abutment type, a large crown-implant ratio (CIR) increased bone strain and stress in the implant components, particularly under oblique loading.

ESTIMATION OF FATIGUE LIFE BY LETHARGY COEFFICIENT USING MOLECULAR DYNAMIC SIMULATION

  • Song, J.H.;Noh, H.G.;Yu, H.S.;Kang, H.Y.;Yang, S.M.
    • International Journal of Automotive Technology
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    • 제5권3호
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    • pp.215-219
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    • 2004
  • A vehicle structure needs to be more precisely analyzed because of complexities and varieties. Structural fatigue which is generated by fluctuations of stresses during the service life of a mechanical system is the primary concern in the structural design for safety. A fatigue life is difficult to obtain in structural components during the service life of mechanical systems since the fluctuating stress contributes to fatigue. This study introduces new procedures to measure the lethargy coefficient and to predict the fatigue life of a mechanical structure by using molecular dynamic simulation. A lethargy coefficient is the total defect-estimating coefficient, which was obtained by using the results of a simple tensile test in this study. With this lethargy coefficient, fatigue life was estimated. The proposed method will be useful in predicting the fatigue life of a structurally-modified vehicle design. The effectiveness of the proposed method using lethargy coefficient measurement to predict the fatigue life of a structure was examined by applying this method to predict the fatigue life of SS41 steel, used extensively as material of vehicle structures. Two types of specimen such as pre-cracked plate and simple plate is discussed. equation of fatigue life using the lethargy coefficient and failure time, both obtained from a simple tensile test, will be useful in engineering. This measurement and prediction technology will be extended for use in analysis of any geometric shapes of modified automotive structures.

카본-페놀 직물복합재료의 층간인장물성 측정기법 (Test Method on Interlaminar Tensile Properties of Carbon Fabric Reinforced Phenolic Composites)

  • 이지형;김형근;이형식;박영채;주세균
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2006년도 제26회 춘계학술대회논문집
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    • pp.81-85
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    • 2006
  • 적층 복합재료를 구조재로 이용할 경우 발생하는 구조적 파단과 두꺼운 원환체 형상의 복합재를 성형할 경우 발생하는 층간파단(interlaminar failures)은 주로 층간 인장응력에 기인하기 때문에 적층 복합재료의 층간인장 물성은 구조해석 시 요구되는 물성이다. 그러나 복합재료의 층간 인장물성은 세계적으로 통일된 시험방법 및 시험규격이 없고 신뢰할 수 있는 물성자료가 없어 자체적인 평가를 수행하여야 한다. 본 논문에서는 국내에서 내열/구조재로 생산되고 있는 카본/페놀 복합재료의 층간 인장물성 비교/평가에 앞서 층간 인장물성의 측정에 대한 시험적 연구를 수행하였다. 시험방법 연구에서는 알루미늄 시편을 이용하여 재료의 탄성한계 내에서 몇 가지 시험을 수행하여 시험방법을 비교 평가하였으며 그 결과로 선정한 시험방법을 복합재료에 적용하였다. 시험의 결과, 복합재 시편의 모든 면에서 같은 경향의 변형률을 얻음에 따라 저 하중에서 파단이 발생하는 복합재료의 층간 인장물성 최적 시험기법을 확보하였다.

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Perforation optimization of hydraulic fracturing of oil and gas well

  • Zhu, Hai Yan;Deng, Jin Gen;Chen, Zi Jian;An, Feng Chen;Liu, Shu Jie;Peng, Cheng Yong;Wen, Min;Dong, Guang
    • Geomechanics and Engineering
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    • 제5권5호
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    • pp.463-483
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    • 2013
  • Considering the influences of fluid penetration, casing, excavation processes of wellbore and perforation tunnels, the seepage-deformation finite element model of oil and gas well coupled with perforating technique is established using the tensile strength failure criterion, in which the user-defined subroutine is developed to investigate the dynamic evolvement of the reservoir porosity and permeability. The results show that the increases of perforation angle and decreases of perforation density lead to a higher fracture initiation pressure, while the changes of the perforation diameter and length have no evident influences on the fracture initiation pressure. As for initiation location for the fracture in wellbore, it is on the wellbore face while considering the presence of the casing. By contrast, the fractures firstly initiate on the root of the tunnels without considering casing. Besides, the initial fracture position is also related with the perforation angle. The fracture initiation position is located in the point far away from the wellbore face, when the perforation angle is around $30^{\circ}$; however, when the perforation angle is increased to $45^{\circ}$, a plane fracture is initiated from the wellbore face in the maximum horizontal stress direction; no fractures was found around perforation tunnels, when the angel is close to $90^{\circ}$. The results have been successfully applied in an oilfield, with the error of only 1.1% comparing the fracture initiation pressure simulated with the one from on-site experiment.

Investigation lateral deformation and failure characteristics of strip coal pillar in deep mining

  • Chen, Shaojie;Qu, Xiao;Yin, Dawei;Liu, Xingquan;Ma, Hongfa;Wang, Huaiyuan
    • Geomechanics and Engineering
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    • 제14권5호
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    • pp.421-428
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    • 2018
  • In deep mining, the lateral deformation of strip coal pillar appears to be a new characteristic. In order to study the lateral deformation of coal-mass, a monitoring method and monitoring instrument were designed to investigate the lateral deformation of strip coal pillar in Tangkou Coalmine with the mining depth of over 1000 m. Because of without influence of repeated mining, the bedding sandstone roof is easy to break and the angle between maximum horizontal stress and the roadway is small, the maximum lateral deformation is only about 287 mm lower than the other pillars in the same coalmine. In deep mining, the energy accumulation and release cause a discontinuous damage in the heterogeneous coal-mass, and the lateral deformation of coal pillar shows discontinuity, step and mutation characters. These coal-masses not only show a higher plasticity but also the high brittleness at the same time, and its burst tendency is more obvious. According to the monitoring results and theoretical calculations, the yield zone of the coal pillar width is determined as 15.6 m. The monitoring results presented through this study are of great significance to the stability analysis and design of coal pillar.

Computation of stress-deformation of deep beam with openings using finite element method

  • Senthil, K.;Gupta, A.;Singh, S.P.
    • Advances in concrete construction
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    • 제6권3호
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    • pp.245-268
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    • 2018
  • The numerical investigations have been carried out on deep beam with opening subjected to static monotonic loading to demonstrate the accuracy and effectiveness of the finite element based numerical models. The simulations were carried out through finite element program ABAQUS/CAE and the results thus obtained were validated with the experiments available in literature. Six simply supported beams were modelled with two square openings of 200 and 250 mm sides considered as opening at centre, top and bottom of the beam. In order to define the material behaviour of concrete and reinforcing steel bar the Concrete Damaged Plasticity model and Johnson-Cook material parameters available in literature were employed. The numerical results were compared with the experiments in terms of ultimate failure load, displacement and von-Mises stresses. In addition to that, seventeen beams were simulated under static loading for studying the effect of opening location, size and shape of the opening and depth, span and shear span to depth ratio of the deep beam. In general, the numerical results accurately predicted the pattern of deformation and displacement and found in good agreement with the experiments. It was concluded that the structural response of deep beam was primarily dependent on the degree of interruption of the natural load path. An increase in opening size from 200 to 250 mm size resulted in an average shear strength reduction of 35%. The deep beams having circular openings undergo lesser deflection and thus they are preferable than square openings. An increase in depth from 500 mm to 550 mm resulted in 78% reduced deflection.

Computational investigation of the comparative analysis of cylindrical barns subjected to earthquake

  • Zandi, Yousef;Shariati, Mahdi;Marto, Aminaton;Wei, Xing;Karaca, Zeki;Dao, Duy Kien;Toghroli, Ali;Hashemi, Mir Heydar;Sedghi, Yadollah;Wakil, Karzan;Khorami, Majid
    • Steel and Composite Structures
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    • 제28권4호
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    • pp.439-447
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    • 2018
  • The structural behaviors of cylindrical barns as a specific engineering structure have been considered as a complicated computing process. The structure design against the earthquake load, to protect by using the code, is an urgency avoiding unexpected damages. The situation has been subjected to the applied design method if there would be no failure across the construction procedures. The purpose of the current study is to clarify the behaviors of cylindrical reinforced concrete barns through the analytic methods across the mass and Lagrangian approaches through the whole outcomes comparison indicating that the isoparametric element obtained from the Lagrangian approach has been successfully applied in the barns earthquake analysis when the slosh effects have been discarded. The form of stress distributions is equal with $s_z$ closed distributions to one another.

설계변수별 연속철근 콘크리트 포장의 피로수명 연구 (Study on Fatigue Life of Continuously Reinforced Concrete Pavement with Design Parameter)

  • 박종섭;강영종
    • 한국방재학회 논문집
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    • 제7권5호
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    • pp.1-10
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    • 2007
  • 초기 설계조건이 반영된 연속철근 콘크리트 포장의 피로수명을 규명하고자 시험체를 제작하여 피로시험을 실시하였다. 유한요소해석 결과분석과 사용되는 재료의 특성을 고려하여 축소된 8개의 시험체를 제작하였다. 피로시험에 앞서서 정적파괴하중 결정과 균열발생 및 진전 상황을 추정하고자 정적하중재하 시험이 실시되었다. 피로시험 결과로부터 초기발생균열의 간격이 증가할수록 피로수명이 증가하는 것을 확인할 수 있었으며, 콘크리트 슬래브 표면 가까이에 철근을 배근한 시험체가 슬래브 중앙에 철근을 배근한 시험체 보다 우수한 피로수명을 나타내었다. 또한, 지반조건의 변화가 균열발생 및 피로수명에 큰 영향을 미치는 것을 확인할 수 있었다. 본 연구의 결과는 국내 고속도로에 건설된 연속철근 콘크리트 포장의 유지보수에 적극 활용될 수 있을 것이다.