• 제목/요약/키워드: Compressive Failure

검색결과 894건 처리시간 0.032초

Hashin 파손이론을 이용한 복합재 볼트체결부의 점진적 파손 해석 및 강도 예측 (Progressive Failure Analysis and Strength Prediction based on Hashin Failure Criterion of Bolted Composite Joint)

  • 김성민;김평화;도성철;김형근;박정선
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.936-938
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    • 2017
  • 본 논문에서는 발사체 및 무기체계의 연소관 등에 적용되고 있는 복합재의 볼트체결부에 대한 점진적 파손 해석을 수행하였다. 해석에 사용된 Hashin 파손 판정식은 복합재 파손모드에 따라 섬유 인장 파손 모드(Fiber tensile failure mode), 섬유 압축 파손 모드(Fiber compressive failure mode), 기지 인장 파손 모드(Matrix tensile failure mode), 기지 압축 파손 모드(Matrix compressive failure mode)의 4가지 모드로 고려되었으며, 이를 이용해 user subroutine인 UMAT을 개발하였다. 점진적 파손 해석을 통해 복합재 볼트체결부에 대한 파손강도를 예측 하였으며, 이를 시편 시험 결과와 비교하였다.

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노치가 있는 콘크리트 실험체의 축압축 강도에 대한 크기효과 (Size Effect on Axial Compressive Strength of Notched Concrete Specimens)

  • 이성태;김봉준;김진근
    • 콘크리트학회논문집
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    • 제12권6호
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    • pp.99-108
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    • 2000
  • The size effect on axial compressive strength in notched concrete specimens was experimentally investigated. Based on the concept of the fracture mechanics and size effect law, theoretical studies for axial compressive failure of concrete were reviewed, and two failure modes of concrete specimens under compression were discussed. In this study, experiments of axial compressive failure, which is one of the two failure modes, was carried out by using cylindrical specimens. Adequate notch length was taken from the experimental result of strength variation based on the notch length. And, by taking various sizes of specimens the size effect on axial compressive strength of concrete was investigated. Also, model equations were suggested by modified size effect law (MSEL). The test results show that size effect appears conspicuously for all series of specimens. Additionally, the effect of initial notch length on axial compressive strength was also apparent.

노치가 있는 콘크리트 공시체의 축압축강도에 대한 크기효과 (Size Effect of Axial Compressive Strength of Concrte in Notched Specimens)

  • 김민욱;김진근;김봉준
    • 한국콘크리트학회:학술대회논문집
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    • 한국콘크리트학회 1999년도 봄 학술발표회 논문집(I)
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    • pp.135-140
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    • 1999
  • The size effect of axial compressive strength of concrete in notched specimens was experimentally investigated. Based on the concept of the fracture mechanics and size effect law, theoretical studies for axial compressive failure of concrete were reviewed, and two failure modes of concrete specimen under compression were discussed. In this study, experiment of axial compressive failure, which is one of the two failure modes, was carried out by using double cantilever fracture specimens. By varying the slenderness of cantilevers and the eccentricity of applied loads with respect to the axis of each cantilever, the size effect of axial compressive strength of concrete was investigated, and predicted by Bazant's size effect law. The test results show that size effect appears conspicuously for all series of specimens. For the eccentricity of loads, the influence of tensile and compressive stress at the notch tip are significant and so that the size effect is varied. In other words, if the influence of tensile stress at the notch tip grows up, the size effect of concrete increases. And the fact that the fracture process zone must be sufficiently secured for more accurate experiment was affirmed.

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Creep characteristics and instability analysis of concrete specimens with horizontal holes

  • Xin, Yajun;Hao, Haichun;Lv, Xin;Ji, Hongying
    • Computers and Concrete
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    • 제22권6호
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    • pp.563-572
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    • 2018
  • Uniaxial compressive strength test and uniaxial compression creep one were produced on four groups of twelve concrete specimens with different hole number by RLW-2000 rock triaxial rheology test system. The relationships between horizontal holes and instantaneous failure stress, the strain, and creep failure stress, the strain, and the relationships between stress level and instantaneous strain, creep strain were studied, and the relationship between horizontal holes and failure mode was determined. The results showed that: with horizontal hole number increasing, compressive strength of the specimens decreased whereas its peak strain increased, while both creep failure strength and its peak strain decreased. The relationships between horizontal holes and compressive strength of the specimens, the peak strain, were represented in quadratic polynomial, the relationships between horizontal holes and creep failure strength, the peak strain were represented in both linear and quadratic polynomial, respectively. Instantaneous strain decreased with stress level increasing, and the more holes in the blocks the less the damping of instantaneous strain were recorded. In the failure stress level, instantaneous strain reversally increased, creep strain showed three stages: decreasing, increasing, and sharp increasing; in same stress level, the less holes the less creep strain rate was recorded. The compressive-shear failure was produced along specimen diagonal line where the master surface of creep failure occurred, the more holes in a block, the higher chances of specimen failure and the more obvious master surface were.

두꺼운 일방향 탄소섬유-에폭시 적층판의 정적 압축 강도 연구 (Static Compressive Strength of Thick Unidirectional Carbon Fiber - Epoxy Laminate)

  • ;;공창덕
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2005년도 추계학술발표대회 논문집
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    • pp.61-65
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    • 2005
  • Existing test methods for thick-section specimens ( 4mm) have not provided precise compressive properties to date for the analysis and design of thick structure. A survey of the failure behaviour of such thick specimens revealed that the failure initiated at the top corner of the specimen and propagated down and across the width of the specimen as premature failure, not typically reported for thin compression specimens. In the current study, the premature failure was successfully avoided during compressive testing and the failure mode was quite similar regardless of increasing specimen thickness and specimen volume. Failure mode was similar regardless of increasing specimen thickness and specimen volume, i.e. brooming failure mode combined with longitudinal splitting, interlaminar cracking, fibre breakage and kinkband formation (fibre microbuckling). Nevertheless, average failure strengths of the specimens decreased with increasing specimen thicnkiness from 2mm to 8mm with the T800/924C system (36% strength reduction) and specimen volumes from scaling factor I to scaling factor 4 with the IM7/8552 system (46% strength reduction). It was revealed from the literature$^{11}$ that the thickness effect and scaling effect arc caused by manufacturing defects such as void content and fibre waviness.

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방사성폐기물 지층처분을 위한 화강암의 열역학적 파괴거동 연구 (A Study on Thermomechanical Failure Behavior of Granites for Radioactive Waste Repository)

  • 양형식;장명환
    • 터널과지하공간
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    • 제6권1호
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    • pp.69-74
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    • 1996
  • High temperature confined compressive tests for thermomechanical failure criteria were carried out for Iksan and Whandeung granites. Authors suggested new polynomial type failure coefficient functions by which conventional Hoek-Brown failure criteria was extended to thermomechanical one. Obtained results are as follow; 1) Failure coefficients, m and s of Hoek and Brown's empirical failure criteria were decreased as temperature increased. 2) Theoretically calculated values by suggested equations and experimented ones by confined compressive test were well coincided.

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Eccentrically compressive behaviour of RC square short columns reinforced with a new composite method

  • Zhang, Fan;Lu, Yiyan;Li, Shan;Zhang, Wenlong
    • Steel and Composite Structures
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    • 제27권1호
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    • pp.95-108
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    • 2018
  • A new composite reinforced method, namely self-compacting concrete filled circular CFRP-steel jacketing, was proposed in this paper. Experimental tests on eight RC square short columns reinforced with the new composite reinforced method and four RC square short columns reinforced with CFS jackets were conducted to investigate their eccentrically compressive behaviour. Nine reinforced columns were subjected to eccentrically compressive loading, while three reinforced columns were subjected to axial compressive loading as reference. The parameters investigated herein were the eccentricity of the compressive loading and the layer of CFRP. Subsequently, the failure mode, ultimate load, deformation and strain of these reinforced columns were discussed. Their failure modes included the excessive bending deformation, serious buckling of steel jackets, crush of concrete and fracture of CFRP. Moreover, these reinforced columns exhibited a ductile failure globally. Both the eccentricity of the compressive loading and the layer of CFRP had a significant effect on the eccentrically compressive behaviour of reinforced columns. Finally, formulae for the evaluation of the ultimate load of reinforced columns were proposed. The theoretical formulae based on the ultimate equilibrium theory provided an effective, acceptable and safe method for designers to calculate the ultimate load of reinforced columns under eccentrically compressive loading.

인장/압축 Broutman Fragmentation시험법과 음향방출을 이용한 단섬유 복합재료의 미세파괴 메커니즘의 연구 (A Study on Microfailure Mechanism of Single-Fiber Composites using Tensile/Compressive Broutman Fragmentation Techniques and Acoustic Emission)

  • Park, Joung-Man;Kim, Jin-Won;Yoon, Dong-Jin
    • Composites Research
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    • 제13권4호
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    • pp.54-66
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    • 2000
  • 탄소섬유/에폭시 복합재료의 계면 및 미세파괴 물성을 인장 fragmentation과 압축 Broutman 두 시험법과 음향방출 시험을 이용하여 평가하였다. Maleic anhydride polymeric coupling agent와 amino-silane를 각각 전기증착법 및 dipping을 통하여 섬유표면에 적용하였다. 두 coupling agents를 사용한 섬유와 기지간의 계면전단강도는 인장 및 압축 두 시험에서 모두 미처리와 비교하여 큰 증가를 나타내었다. 인장시험 동안에, 원추모양의 섬유파단과 기지의 cracking 그리고 부분적인 interlayer failure로 이루어진 전형적인 미세파괴 형태가 발생하였다. 이에 비하여, 압축시험에서는 부러진 섬유의 끝에서 대각선 방향이 슬립거동이 관찰되었다. 주어진 두 힘의 하중상태에서 섬유의 파단은 항복점 전후 부근에서 일어났다. 음향방출분포는 인장에서 섬유표면 처리와 미처리의 두 조건에서 미세파괴 신호가 잘 분리되었으며, 한편, 압축에서는 signal이 다소 중복되어 나타났다. 이는 탄소섬유의 인장력/압축력 간의 파괴에너지 차이에 기인한다고 고려된다. 탄소와 basalt 섬유복합재료의 섬유파단 waveform의 최대 voltage는 압축보다 인장시험에서 상당히 크게 나타났으며, 이들은 음향방출시험으로 파괴에너지 차이를 명확히 비교 및 확인할 수 있었다.

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T300/924C 탄소섬유/에폭시 복합재 적층판의 이차원 압축 강도의 크기효과 및 좌굴방지장치의 영향 (Two Dimensional Size Effect on the Compressive Strength of T300/924C Carbon/Epoxy Composite Plates Considering Influence of an Anti-buckling Device)

  • 공창덕;방조혁;이정환
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2002년도 추계학술발표대회 논문집
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    • pp.88-91
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    • 2002
  • The two dimensional size effect of specimen gauge section (length x width) was investigated on the compressive behavior of a T300/924 [45/-45/0/90]3s, carbon fiber-epoxy laminate. A modified ICSTM compression test fixture was used together with an anti-buckling device to test 3mm thick specimens with a 30$\times$30, 50$\times$50, 70$\times$70, and 90mm$\times$90mm gauge length by width section. In all cases failure was sudden and occurred mainly within the gauge length. Post failure examination suggests that $0^{\circ}$ fiber microbuckling is the critical damage mechanism that causes final failure. This is the matrix dominated failure mode and its triggering depends very much on initial fiber waviness. It is suggested that manufacturing process and quality may play a significant role in determining the compressive strength. When the anti-buckling device was used on specimens, it was showed that the compressive strength with the device was slightly greater than that without the device due to surface friction between the specimen and the device by pretoque in bolts of the device. In the analysis result on influence of the anti-buckling device using the finite element method, it was found that the compressive strength with the anti-buckling device by loaded bolts was about 7% higher than actual compressive strength. Additionally, compressive tests on specimen with an open hole were performed. The local stress concentration arising from the hole dominates the strength of the laminate rather than the stresses in the bulk of the material. It is observed that the remote failure stress decreases with increasing hole size and specimen width but is generally well above the value one might predict from the elastic stress concentration factor. This suggests that the material is not ideally brittle and some stress relief occurs around the hole. X-ray radiography reveals that damage in the form of fiber microbuckling and delamination initiates at the edge of the hole at approximately 80% of the failure load and extends stably under increasing load before becoming unstable at a critical length of 2-3mm (depends on specimen geometry). This damage growth and failure are analysed by a linear cohesive zone model. Using the independently measured laminate parameters of unnotched compressive strength and in-plane fracture toughness the model predicts successfully the notched strength as a function of hole size and width.

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Experimental research on the failure mechanism of foam concrete with C-Channel embedment

  • Liu, Dianzhong;Wang, Fayu;Fu, Feng;Wang, He
    • Computers and Concrete
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    • 제20권3호
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    • pp.263-273
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    • 2017
  • An experimental investigation is carried out on the failure mechanism of foam concrete with cold formed steel double C-Channels embedment. The foam concrete is made of cement and fly ash with a compressive strength between 9 and 24 MPa with different densities. Forty-eight tests have been carried out in four groups of specimens with various embedment depths of the steel in the concrete. Four modes of failure are observed, which include the independent failure of the C-Channels with and without a concrete block inside the channel as well as the combined failure of the two channels, and the failure of the extrusion block. A theoretical model has been developed to understand the failure process. The peak compressive force applied onto the C-Channels that causes failure is calculated. It is concluded that the failure involves independent slippage between two C-Channels, and the steel and the foam concrete blocks inside the C-Channels. A method to calculate the peak force is also developed based on the test results. The calculations also show that the shear strength of the foam concrete is about 8% of the compressive strength with ${\alpha}$ coefficient of 0.4 between the steel and concrete.