• 제목/요약/키워드: Uniaxial stress

검색결과 571건 처리시간 0.026초

유한요소법에 의한 직방성재료 내 균열의 응력확대계수 결정 (Determination of Stress Intensity Factor for the Crack in Orthotropic Materials Using the Finite Element Method)

  • 조형석;강석진;이성근;임원균
    • 한국전산구조공학회논문집
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    • 제17권1호
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    • pp.59-65
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    • 2004
  • 응력확대계수는 균열진전경로의 수치해석적 연구에서 널리 사용되고 있다. 그러나 많은 경우에서 균열선단주위 응력의 급수전개식 중 이어지는 항은 정량적으로 중요하다. 따라서 본 연구에서는 이의 항을 계산하기 위하여 등매개 2차특이요소를 이용한 유한요소해석을 수행하였다. 일례로 단축하중을 받는 무한 직방성체 내 경사균열에 대하여 균열요소크기와 균열경사각을 달리 주어 가며 해석을 수행하였으며, 수치해석결과는 이론해와 비교하여 잘 일치하고 있다.

Ti-42.5at.%Ni-2.0at.%Cu합금의 인장 및 압축에 따른 형상기억특성에 관한 연구 (A Study on the Shape Memory Characteristic Behaviors of Ti-42.5at.%Ni-2.0at.%Cu Alloys in Tension and Compression Condition)

  • 우흥식;조재환;박용규
    • 한국안전학회지
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    • 제24권5호
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    • pp.1-5
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    • 2009
  • NiTiCu alloys can produce a large force per unit volume and operate with a simple mechanism. For this reasons, it has been widely studied for application as a micro actuator. So in this study, one-way and two way shape memory effects of Ti-42.5at%Ni-2.0at%Cu alloys are studied. In the case of one-way shape memory effects, shape memory recoverable stress and strain of this alloys were measured by means of tension and compression tests under constant temperature. The strains by tension and compression stress were perfectly recovered by heating at any testing conditions also shape memory recoverable stress increased to 116 MPa in tension tests and to 260 MPa in compression tests. In the case of two-way shape memory effects, transformation temperatures from thermal cycling under constant uniaxial applied tension and compression loads linearly increased by increasing external loads and their maximum recoverable strain is 3.8% at 100MPa tensile condition and 2.2% at 125 MPa compression condition.

Comparison of the Stress Concentration Factors for GFRP Plate having Centered Circular Hole by Three Resource-Conserving Methods

  • Gao, Zhongchen;Park, Soo-Jeong;Kim, Yun-Hae
    • Composites Research
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    • 제29권6호
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    • pp.388-394
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    • 2016
  • Fiber reinforced plastic (FRP) composites have drawn increasing attentions worldwide for decades due to its outstanding properties. Stress concentration factor (SCF) as an essential parameter in materials science are critically considered in structure design and application, strength assessment and failure prediction. However, investigation of stress concentration in FRP composites has been rarely reported so far. In this study, three resource-conserving analyses (Isotropic analysis, Orthotropic analysis and Finite element analysis) were introduced to plot the $K_T^A-d/W$ curve for E-glass/epoxy composite plate with the geometrical defect of circular hole placed centrally. The plates were loaded to uniaxial direction for simplification. Finite element analysis (FEA) was carried out via ACP (ANSYS composite prepost module). Based on the least squares method, a simple expression of fitting equation could be given based on the simulated results of a set of discrete points. Finally, all three achievable solutions were presented graphically for explicit comparison. In addition, the investigation into customized efficient SCFs has also been carried out for further reference.

5% 크롬 냉간 압연용 작업롤의 피로손상 평가에 대한 연구 (Assessment of fatigue damage in 5% chrome cold rolling work roll)

  • 곽길준;김광수;이시우;여원구;박영철
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 추계학술대회논문집A
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    • pp.316-321
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    • 2000
  • The role of fatigue on the surface damage of 5% chrome cold milling work roll is evaluated. Uniaxial and torsional fatigue tests are carried out, and the baseline data for fatigue life evaluation are established. An appropriate multiaxial fatigue parameter is developed from the fatigue data. Fatigue tests are also performed under compressive mean stresses, and a mean stress model is formulated. A computer program is developed to assess the interaction of fatigue and grinding of the roll. The fatigue damage is computed for selected servicing conditions. It is found that the fatigue damage can be an important issue when the effect of mean stress is ignored, however the fatigue damage is negligibly small when the effect of mean stress including the residual stresses currently used is fully accounted. The result indicates that spalling due to the growth of thermal shock cracks is more important than fatigue damage in roll surface failure.

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ETFE 막재에 대한 인장실험과 크리프 실험 (Tensile Test and Creep Tests of ETFE Membrane)

  • 김재열;강주원
    • 한국공간구조학회논문집
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    • 제10권3호
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    • pp.57-64
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    • 2010
  • 본 논문에서는 세 종류의 ETFE 막재에 대한 단축인장실험을 수행하였다. 이 실험에서 얻은 변형도-변위 곡선을 분석함으로써 항복응력, 두 번째 항복응력, 탄성계수, 두 번째 탄성계수, 그리고 세 번째 탄성계수를 얻게 되었다. 아울러, 탄성 단계와 항복 단계, 소성유동 단계에서 각각 ETFE 막재의 사이클 하중시험을 진행하여, 잔여변형률, 응력 이완, 하중 변화(재하/제하) 중 ETFE 막재의 탄성 변화 등을 알아본다. 재료의 크리프시험에서는 25, 40, 60$^{\circ}C$의 시험온도와 3, 6, 9MPa의 인장 응력 하에서 크리프시험의 시간은 24시간으로 설정하였다.

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간접인장강도시험을 통한 이방성 암석의 인장강도 특성 (Characterization of Tensile Strength of Anisotropic Rock Using the Indirect Tensile Strength Test)

  • 김영수;정성관;최정호
    • 한국지반공학회논문집
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    • 제18권5호
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    • pp.133-141
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    • 2002
  • 암반파괴의 가장 큰 영향을 미치는 인장강도는 등방의 암석과 횡등방의 암석의 경우는 분명히 다를 것이다. 본 논문에서는 일축압축강도시험에서 횡등방 암석의 탄성정수를 구하고, 간접인장강도시험을 통하여 횡등방 암석의 인장강도와 인장파괴 거동을 분석하였다. 일축압축시험에서 구한 이방성 탄성정수와 간접인장강도시험에서 얻어진 변형률로 시료중앙의 응력집중계수를 구하여, 등방으로 가정하여 구한 인장강도 값과 이방성일때의 인장강도 값을 비교 분석하였다. 실험 결과 횡등방성 암석의 응력집중계수는 층리면의 각도에 따라서 등방재료의 응력집중계수와는 크거나 작은 값을 나타내었다. 횡등방 암석의 인장강도 산정시 등방의 응력집중계수를 사용하는 것은 층리면이 이루는 각도에 따라 인장강도의 과대 혹은 과소 평가됨을 알 수 있었다.

Multi-scale Progressive Failure Analysis of Triaxially Braided Textile Composites

  • Geleta, Tsinuel N.;Woo, Kyeongsik
    • International Journal of Aeronautical and Space Sciences
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    • 제18권3호
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    • pp.436-449
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    • 2017
  • In this paper, the damage and failure behavior of triaxially braided textile composites was studied using progressive failure analysis. The analysis was performed at both micro and meso-scales through iterative cycles. Stress based failure criteria were used to define the failure states at both micro- and meso-scale models. The stress-strain curve under uniaxial tensile loading was drawn based on the load-displacement curve from the progressive failure analysis and compared to those by test and computational results from reference for verification. Then, the detailed failure initiation and propagation was studied using the verified model for both tensile and compression loading cases. The failure modes of each part of the model were assessed at different stages of failure. Effect of ply stacking and number of unit cells considered were then investigated using the resulting stress-strain curves and damage patterns. Finally, the effect of matrix plasticity was examined for the compressive failure behavior of the same model using elastic, elastic - perfectly plastic and multi-linear elastic-plastic matrix properties.

과냉각 구간에서 Cu-계 아몰퍼스 복합재의 변형거동 (Deformation behavior of Copper Amorphous Composites in Super Cooled Liquid Region)

  • 박은수;김지수;김휘준;배정찬;허무영
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 2005년도 춘계학술대회 논문집
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    • pp.279-282
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    • 2005
  • Composites comprising various volume fractions of crystalline nickel and bulk amorphous (BA) were produced by means of electroless coating of nickel on BA powder of $Cu_{54}Ni_6Zr_{22}Ti_{18}$ and subsequent spark plasma sintering (SPS) of coated BA powder. The flow curves of composites at various temperatures in the supercooled liquid region were determined by the uniaxial compression test with various strain rates. During compression at $450^{\circ}C$ with $\dot{\varepsilon}=2\times10^{-3}$, the monolithic BA sample and crystalline-BA composites displayed the superplastic deformation with $\varepsilon>1.4$. At temperatures above $460^{\circ}C$, the stress-strain curve of the monolithic BA sample depicted a sharp peak stress and a fellowing stress drop due to cracking, while those of the crystalline-BA composites displayed work-hardening up to the imposed strain. FEM analysis indicated that a fairly homogeneous strain state prevailed throughout the composite, while a higher level of stress was obtained in a harder BA.

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아라미드 스트랩으로 프리스트레싱 횡구속된 RC 원형기둥의 일축압축거동에 관한 실험적 연구 (An Experimental Study on Uniaxial Compressive Behavior of RC Circular Columns Laterally Confined with Prestressing Aramid Fiber Strap)

  • 한상훈;홍기남;이재범
    • 콘크리트학회논문집
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    • 제21권2호
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    • pp.159-168
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    • 2009
  • 본 연구에서는 기존의 연구방법을 개선한 프리스트레스가 도입된 아라미드 스트랩으로 횡 구속된 RC 원형기둥의 일축압축 거동에 대하여 강도와 변위에 의한 강성 및 구속효과에 대하여 연구하였으며, 그 프리스트레싱 보강방법 및 과정에 대하여 비교적 상세히 소개하였다. 이 방법으로 보강된 기둥의 파괴형태는 초기 능동 구속압의 작용으로 인하여 변위 증가율이 매우 낮으며 이후 최종 파괴시까지도 그 형상이 유지되는 매우 안정적인 파괴형태를 보이게 된다. 파괴하중 비교 결과 일반 RC 기둥과 비교하여 73% 이상 강도증진 효과를 나타내었다. 또한 변형 증가율이 매우 작으며 이로 인한 변위구속효과가 매우 우수함을 확인할 수 있었다. 기존의 보강방법 (CFS, GFS)과의 비교를 통하여, 상대적으로 작은 면적으로 우수한 강도증진을 보이며 강성증가로 인한 구속효과 역시 우수하며 체적 증가율도 팽창하지 않는 결과를 보였다. 특히, 콘크리트 팽창 이후부터 발휘되는 기존 방법의 구속효과와는 달리, 초기부터 도입되는 프리스트레스트 긴장력에 의한 초기변형 구속효과가 매우 탁월하며, 최종 파괴시까지 체적 변형률이 팽창하지 않는 안정적인 결과를 나타낸다.

An experimental study on fracture coalescence characteristics of brittle sandstone specimens combined various flaws

  • Yang, Sheng-Qi
    • Geomechanics and Engineering
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    • 제8권4호
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    • pp.541-557
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    • 2015
  • This research aims to analyze the fracture coalescence characteristics of brittle sandstone specimen ($80{\times}160{\times}30mm$ in size) containing various flaws (a single fissure, double squares and combined flaws). Using a rock mechanics servo-controlled testing system, the strength and deformation behaviours of sandstone specimen containing various flaws are experimentally investigated. The results show that the crack initiation stress, uniaxial compressive strength and peak axial strain of specimen containing a single fissure are all higher than those containing double squares, while which are higher than those containing combined flaws. For sandstone specimen containing combined flaws, the uniaxial compressive strength of sandstone increase as fissure angle (${\alpha}$) increases from $30^{\circ}$ to $90^{\circ}$, which indicates that the specimens with steeper fissure angles can support higher axial capacity for ${\alpha}$ greater than $30^{\circ}$. In the entire deformation process of flawed sandstone specimen, crack evolution process is discussed detailed using photographic monitoring technique. For the specimen containing a single fissure, tensile wing cracks are first initiated at the upper and under tips of fissure, and anti-tensile cracks and far-field cracks are also observed in the deformation process; moreover anti-tensile cracks usually accompanies with tensile wing cracks. For the specimen containing double squares, tensile cracks are usually initiated from the top and bottom edge of two squares along the direction of axial stress, and in the process of final unstable failure, more vertical splitting failures are observed in the ligament region. When a single fissure and double squares are formed together into combined flaws, the crack coalescence between the fissure tips and double squares plays a significant role for ultimate failure of the specimen containing combined flaws.