• 제목/요약/키워드: failure strain

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암석의 성인별 한계변형률 특성에 관한 연구 (A study on critical strain properties of intact rock due to Petrogenesis)

  • 김영수;박시현;김대만;신지섭;한희수
    • 한국지반공학회:학술대회논문집
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    • 한국지반공학회 2009년도 춘계 학술발표회
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    • pp.1133-1138
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    • 2009
  • This study was conducted in order to know the internal application of the critical strain graph. To evaluate critical strain graph, we carried out an uniaxial compression test with some of internal rocks: sandstone, shale, weathered granite, and pink granitic. Based on the uniaxial compression test, we deduced relations among critical strain, failure strain, uniaxial compression strength and modulus of elasticity. As a result, the study has found out the rocks, which have been tested, can be possibly evaluated by critical strain graph.

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Localized failure in damage dynamics

  • Do, Xuan Nam;Ibrahimbegovic, Adnan;Brancherie, Delphine
    • Coupled systems mechanics
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    • 제4권3호
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    • pp.211-235
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    • 2015
  • In this work we present a one-dimensional damage model capable of representing the dynamic fracture for elastodamage bar with combined hardening in fracture process zone - FPZ and softening with embedded strong discontinuities. This model is compared with another one we recently introduced (Do et al. 2015) and it shows a good agreement between two models. Namely, it is indicated that strain-softening leads to a sensitivity of results on the mesh discretization. Strain tends to localization in a single element which is the smallest possible area in the finite element simulations. The strain-softening element in the middle of the bar undergoes intense deformation. Strain increases with increasing mesh refinement. Strain in elements outside the strain-softening element gradually decreases to zero.

순수전단이 작용하는 RC막판넬의 전단변형률 증폭 (Shear Strain Big-Bang of RC Membrane Panel Subjected to Shear)

  • 정제평
    • 대한토목학회논문집
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    • 제35권1호
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    • pp.101-110
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    • 2015
  • 최근 Hsu는 전단시험장치를 이용해 순수전단이 작용하는 9개 RC패널요소의 전단시험을 수행하였다(ACI 1997). 최신 트러스모델(수정압축장이론, 회전각연성트러스모델)은 평형조건과 적합조건 그리고 2축 상태에서 RC 막판넬의 연성 응력-변형률 관계를 이용하여 2중 루프의 시행착오방법으로 복잡한 비선형해석을 수행하고 있다. 본 연구는 스트럿과 타이의 파괴기준에 기반한 개선된 모어변형적합방법을 사용해 효율적인 알고리즘을 제안하였고, 이 알고리즘을 이용하여 Hsu가 실험한 전단이력 해석을 빠른 수렴속도로 개선한 것이다. 해석결과에 의하면 전단변형률 증폭상태의 전단변형에너지는 주압축 응력-변형률에 크게 지배받는 것으로 나타났다.

비선형 해석을 통한 보강된 RC 보의 거동 예측 (Behavior Prediction of Strengthened! Reinforced! Concrete Beam using Nonlinear Analysis)

  • 박중열;황선일;조홍동;한상훈
    • 한국콘크리트학회:학술대회논문집
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    • 한국콘크리트학회 2003년도 봄 학술발표회 논문집
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    • pp.561-566
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    • 2003
  • In this study, to predict the behavior of RC beam strengthened with Carbon fiber reinforced polymer(CFRP) plate, analytical program considering material non-linearity is developed. Strain compatibility and force equilibrium are applied and internal forces of constitutive material are calculated using nonlinear stress-strain relationship. Also, to certainty the reliability of analytical program, deflection, strain of CFRP plate, change of neutral axis on cross section and crack distribution at failure are compared with those of experiment, and each results are almost coincident.

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Flexural performance of composite sandwich wall panels with foamed concrete

  • Lei Li;Wei Huang;Zhengyi Kong;Li Zhang;Youde Wang;Quang-Viet Vu
    • Steel and Composite Structures
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    • 제52권4호
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    • pp.391-403
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    • 2024
  • The flexural behavior of composite sandwich wall panels with different thicknesses, numbers of holes, and hole forms, and arrangement form of longitudinal steel bar (uniform type and concealed-beam type) are investigated. A total of twelve composite sandwich wall panels are prepared, utilizing modified polystyrene particles mixed with foam concrete for the flexural performance test. The failure pattern of the composite sandwich wall panels is influenced by the extruded polystyrene panel (XPS) panel thickness and the reinforcement ratio in combination, resulting in both flexural and shear failure modes. Increasing the XPS panel thickness causes the specimens to transition from flexural failure to shear failure. An increase in the reinforcement ratio leads to the transition from flexural failure to shear failure. The hole form on the XPS panel and the steel bar arrangement form affect the loading behavior of the specimens. Plum-arrangement hole form specimens exhibit lower steel bar strain and deflection compared to linear-arrangement hole form specimens. Additionally, specimens with concealed beam-type steel bar display lower steel bar strain and deflection than uniform-type steel bar specimens. However, the hole form and steel bar arrangement form have a limited impact on the ultimate load. Theoretical formulas for cracking load are provided for both fully composite and non-composite states. When compared to the experimental values, it is observed that the cracking load of the specimens with XPS panels closely matches the calculations for the non-composite state. An accurate prediction model for the ultimate load of fully composite wall panels is developed. These findings offer valuable insights into the behavior of composite sandwich wall panels and provide a basis for predicting their performance under various design factors and conditions.

Micromechanical failure analysis of composite materials subjected to biaxial and off-axis loading

  • Ahmadi, Isa
    • Structural Engineering and Mechanics
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    • 제62권1호
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    • pp.43-54
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    • 2017
  • In this study, the failure behavior of composite material in the biaxial and off-axis loading is studied based on a computational micromechanical model. The model is developed so that the combination of mechanical and thermal loading conditions can be considered in the analysis. The modified generalized plane strain assumption of the theory of elasticity is used for formulation of the micromechanical modeling of the problem. A truly meshless method is employed to solve the governing equation and predict the distribution of micro-stresses in the selected RVE of composite. The fiber matrix interface is assumed to be perfect until the interface failure occurs. The biaxial and off-axis loading of the SiC/Ti and Kevlar/Epoxy composite is studied. The failure envelopes of SiC/Ti and Kevlar/Epoxy composite in off-axis loading, biaxial transverse-transverse and axial-transverse loading are predicted based on the micromechanical approach. Various failure criteria are considered for fiber, matrix and fiber-matrix interface. Comparison of results with the available results in the litreture shows excellent agreement with experimental studies.

굴진장을 고려한 얕은 터널파괴거동에 대한 모형실험 및 수치해석 (Model Test and Numerical Analysis for Failure Behaviour of Shallow Tunnel Considering Unsupported Tunnel Length)

  • 김영민
    • 터널과지하공간
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    • 제15권6호
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    • pp.400-410
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    • 2005
  • 토사지반에서 얕은 터널을 굴착하는 경우, 터널 막장부의 파괴 메카니즘이 터널 안정성에 큰 영향을 미친다. 본 논문에서는 일련의 굴진장을 고려한 2차원 종 방향 터널 모형 실험을수행하였다. 그 결과 얕은 터널의 파괴 메카니즘은 굴진장이 길어질수록 파괴모드 1에서 파괴모드 2로 변하는 것을 알 수 있었다. 또한, 모형실험결과와 수치해석을 비교하여 터널에 작용하는 최소 지보압과 진행성 파괴 거동에 대하여 분석하였다.

적층목질재(積層木質材)(Glulam)의 중립축(中立軸)과 강도적(强度的) 성질(性質)에 관한 연구(硏究) (Study on the Neutral Axis of Glulam and its Mechanical Properties)

  • 박헌
    • Journal of the Korean Wood Science and Technology
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    • 제18권3호
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    • pp.42-52
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    • 1990
  • In this study, thick 24mm glulams were composed of thick. 3, 4, 6, 8mm Larch laminas to study that the theoretical analysis and the experimental analysis regarding the location of neutral axis of the glulams were compared, and to study on the effect of location of neutral axis on mechanical properties of glulam. The variation of location of neutral axis after proportional limit(or elastical limit) was studied to offer basic data to make the better composition method of glulam. The result obtained can be summarized as follows: 1. The theoretical neutral axis was 0.547 in solid wood, and also 0.547 in glulams because glulams were composed of only Larch laminas. 2. In solid wood, the deviation of the theoretical and the experimental neutral axis location was 0.1%, But in glulams, the deviation from-12.2% to + 7.8% showed nonuniform pattern but no large deviation. Because laminas was only of Larch and so the mechanical properties of laminas were monotonous. 3. The neutral axis exerted no influance on the elasticity of glulam, which meaned that the maximum shear strength in the neutral axis showed no influance on elasticity limit. 4. The only minutely lower elasticities of glulam than that of solid wood were shown. This was because of influance of glue lines of glulam on the elasticlties. 5. The failure type of glulam was wholly simple tension failure and the horizontal shear failure near neutral axis was not taken place, which was that glue line was complete in bonding and the strength of the lamina was not various but uniform. 6. The ratio of tension strain($^{\varepsilon}t$) I compression strain($^{\varepsilon}c$) initially showed uniform level After the elasticity limit. the ratio was increased with the flow of time and so the tension strain was more increased than compression strain. So this proved tension lamination technique, which is that the mechanical properties of glulam could be improved, if the lamina of more superior strength would he added on the bottom side of the glulam.

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연약지반 보강성토에서 섬유보강재 소요인장강도의 결정 (The Determination of Required Tensile Strength of Geosynthetic Reinforcements for Embankment on Soft Ground)

  • 이광열;황재홍;구태곤
    • 한국지반공학회논문집
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    • 제19권6호
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    • pp.379-385
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    • 2003
  • 기존의 섬유보강성토제체의 설계에서 보강재의 변형을 고려하지 않고 연직응력을 보강재의 인장강도로 사용함으로써, 흙구조물의 파괴응력에 대응하는 보강재의 한계응력산정과 그에 따른 보강재의 규격결정이 불가능했다. 보강재에 의해 보강된 성토제체의 파괴면에서 보강재와 흙의 거동은 초기응력단계에서는 일체로서 거동하지만 응력의 증가에 따라 변형량의 차이가 증가한다. 이러한 문제는 흙구조물의 보강재설계에서 중요한 요소로서 보강효과에 큰 영향을 미칠 수 있다. 본 연구에서는 연약지반위에 PET Mat로 보강한 성토제체의 보강재 설계 시 파괴면상의 보강재 설치위치에서 흙과 보강재의 변형량을 고려한 설계방법을 제시하였다. 연구결과에 의하면, 허용안전율을 확보하는 범위내에서 예상파괴면상의 보강재 설치위치에서의 보강재의 인장강도는 흙의 응력 이상이어야 하며, 흙의 변형링${\Delta S}$과 보강재의 변형량${\Delta G}$이 일체로 거동하는 보강재의 소요인장강도를 보강재의 설계인장강도로서 결정하는 것이 합리적이고 경제적인 것으로 평가되었다.

압축성(壓縮性) 모래의 3차원(次元) 변형거동(變形擧動) (Three Dimensional Deformation Behaviour of Compressible Sand)

  • 박병기;정진섭;임성철
    • 대한토목학회논문집
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    • 제10권3호
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    • pp.107-113
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    • 1990
  • 압축성(壓縮性) 모래를 사용하여 주응력(主應力)을 각기 독립적으로 조절할 수 있는 입방체삼축시험(立方體三軸試驗)을 하였다. 그 결과 초기(初期) 변형계수(變形係數)는 b값의 증가와 더불어 증가하고 중간주응력(中間主應力)이 b값이 적을 때는 주변형율간(主變形率間)의 거동(擧動)에 영향을 미치지 못하고 배수(排水) 경우는 b=0.3, 비배수(非排水)경우는 b=0.6 값에서부터 b값이 커질수록 최대주변형율(最大主變形率)(${\varepsilon}_1$) 값이 더 적은 값에서 파괴(破壞)된다. 파괴시(破壞時) 소성변율(塑性變形率) 중분벡터의 방향은 배수조건(排水條件)에 무관하고 직교조건은 3축면(三軸面)에서는 만족되지 않으나 팔면체면(八面體面)에서는 만족되는 재료(材料)임을 알았다.

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