• 제목/요약/키워드: Critical Energy Release Rate

검색결과 63건 처리시간 0.03초

CLS 시편의 탄성일인자 유도 및 이를 적용한 열가소성 Graphite/Peek 복합재의 파괴인성 $G_c$ 측정 (Elastic Work Factor of CLS Specimen and Determination of $G_c$ for Graphite/Peek Composites by Using the Elastic Work Factor)

  • 이경엽
    • 대한기계학회논문집A
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    • 제20권9호
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    • pp.2792-2799
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    • 1996
  • It was shown in the previous study that the numerically derived elastic work factor for CLS specimen was independent of fiber direction for a unidirectional case. Also, it was proposed the elastic work factor could be used to determine energy release rate from a single test record. In the present study, elastic work factor was derived from a simple beam theory to investigate its dependence on material property and geometric condition. Also, the elastic work factor of CLS specimen was applied experimentally to determine critical energy release rate in order to prove its validity determining critical energy release rate from a single specimen. For this purpose, critical energy release rate determined using the elastic work factor was compared with that determined by the compliance method. The results showed that while elastic work factor is affected by $t_2/t_1$ and $L_2/L_1$ it is independent of fiber angle for a unidirectional case. It was also found that critical energy release rates determined by both methods are comparable each other, thus elastic work factor approach can be used to determine energy release rate from a single test specimen.

유리-탄소 하이브리드 복합재료의 파괴인성에 관한 연구 (A Study on the Fracture Toughness of Glass-Carbon Hybrid Composites)

  • 노호섭;고성위
    • 수산해양기술연구
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    • 제28권3호
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    • pp.295-305
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    • 1992
  • The critical strain energy release rate and the failure mechanisms of glass-carbon epoxy resin hybrid composites are investigated in the temperature range of the ambient temperature to 8$0^{\circ}C$. The direction of laminates and the volume fraction are [(+45, -45, 0, 0) sub(2) ] sub(s), 50%, respectively. The major failure mechanisms of these composites are studied using the scanning electron microscope for the fracture surface. Results are summarized as follows: 1) The critical strain energy release rate shows a maximum at ambient temperature and it tends to decrease as temperature goes up. 2) The critical strain energy release rate increases as the content of glass increases, and especially shows dramatic increase for the high glass fiber content specimens. 3) Major failure mechanisms can be classfied such as localized shear yielding, fiber-matrix debonding, matrix micro-cracking, and fiber pull-out and/or delamination.

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에너지 방출률에 의한 접착이음의 계면균열에 대한 파괴인성의 평가 (Evaluation of Fracture Toughness by Energy Release Rate for Interface Crack in Adhesively Bonded Joints)

  • 정남용;이명대;강삼근
    • 대한기계학회논문집A
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    • 제24권9호
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    • pp.2174-2183
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    • 2000
  • In this paper, the evaluation method of interfacial fracture toughness to apply the fracture toughness was investigated in adhesively bonded joints of AI/Ced./A1. Four types of adhesively bonded double-cantilever beam(DCB) joints with the interface crack were prepared for the test of interfacial fracture toughness. The experiments to measure the interfacial fracture toughness were performed under the various mixed-mode conditions. The critical energy release rate, Gc, was obtained by the experimental measurement of compliances. From the experimental results, the interfacial fracture toughness for the mixed-mode specimens is well characterized by the energy release rate, and the method of strength evaluation by the interfacial fracture toughness was discussed in adhesively bonded joints.

흑연/에폭시 복합재료의 혼합모우드 층간분리 해석 (Analysis of Mixed Mode Delamination in Graphite/Epoxy Composite)

  • 염영진;유희
    • 한국자동차공학회논문집
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    • 제4권4호
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    • pp.171-178
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    • 1996
  • DCB(pure mode I) and CLS(mixed mode) tests were performed to investigate the effect of fracture mode on the interlaminar fracture of composite laminate. Mode I critical strain energy release rate was found to be $133J/m^2$ from the DCB test and total strain energy release rate decreased from $1, 270J/m^2$ as thickness ratio(tl/t) varied from 0.333 to 0.667 from the crease from the CLS test. Crack length had no effect on the total strain energy release rate and load was almost constant during the crack growth of the specimen which had the specific thickness ratio. Crack initiated when the stress of the strap ply reached constant stress $42kgf/mm^2$ which was found to be independent of the thickness ratio.

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표면처리된 탄화규소강화 에폭시 복합재료의 GIIC 특성 (A Study on Critical Strain Energy Release Rate Mode II of Chemically Treated SiC-filled Epoxy Composites)

  • 박수진;오진석
    • 접착 및 계면
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    • 제6권4호
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    • pp.1-6
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    • 2005
  • 본 실험에서는 화학적 표면처리된 탄화규소의 첨가가 탄화규소(SiC)/에폭시 복합재료의 critical strain energy release rate mode II ($G_{IIC}$) 특성에 미치는 영향에 대하여 알아보았으며, 표면처리된 SiC의 표면특성은 산 염기도와 FT-IR을 사용하여 알아보았다. 또한 복합재료의 기계적 계면물성은 $G_{IIC}$를 통하여 알아보았다. 실험결과, 산성 용액으로 표면처리한 SiC (A-SiC)의 표면 산도가 염기성(B-SiC) 또는 표면처리 하지 않은 SiC (V-SiC)보다 높으며, $G_{IIC}$의 크랙저항 특성은 A-SiC가 향상되었는데, 이러한 결과는 SiC 충전재와 에폭시 수지간의 분자간 계면결합력의 향상 때문으로 판단된다.

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Effect of Atmospheric Plasma Treatment of Carbon Fibers on Crack Resistance of Carbon Fibers-reinforced Epoxy Composites

  • Park, Soo-Jin;Oh, Jin-Seok;Rhee, Kyong-Yop
    • Carbon letters
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    • 제6권2호
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    • pp.106-110
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    • 2005
  • In this work, the effects of atmospheric oxygen plasma treatment of carbon fibers on mechanical interfacial properties of carbon fibers-reinforced epoxy matrix composites was studied. The surface properties of the carbon fibers were determined by acid/base values, Fourier-transform infrared spectrometer (FT-IR), and X-ray photoelectron spectroscopy (XPS) analyses. Also, the crack resistance properties of the composites were investigated in critical stress intensity factor ($K_{IC}$), and critical strain energy release rate mode II ($G_{IIC}$) measurements. As experimental results, FT-IR of the carbon fibers showed that the carboxyl/ester groups (C=O) at 1632 $cm^{-1}$ and hydroxyl group (O-H) at 3450 $cm^{-1}$ were observed for the plasma treated carbon fibers, and the treated carbon fibers had the higher O-H peak intensity than that of the untreated ones. The XPS results also indicated that the $O_{1S}/C_{1S}$ ratio of the carbon fiber surfaces treated by the oxygen plasma led to development of oxygen-containing functional groups. The mechanical interfacial properties of the composites, including $K_{IC}$ (critical stress intensity factor) and $G_{IIC}$ (critical strain energy release rate mode II), were also improved for the oxygen plasma-treated carbon fibersreinforced composites. These results could be explained that the oxygen plasma treatment played an important role to increase interfacial adhesions between carbon fibers and epoxy matrix resins in our composite system.

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저속 충격시 PVC/MBS재료의 파괴특성에 관한 연구 (A Study on Fracture Parameters for PVC/MBS Composites under Low Velocity Impact)

  • 최영식;박명균;박세만
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2002년도 추계학술대회 논문집
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    • pp.837-840
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    • 2002
  • An analysis method for rubber toughened PVC is suggested to evaluate critical dynamic strain energy release rates($G_c$) from the Charpy impact energy measurements. An instrumented Charpy impact tester was used to extract ancillary information concerning fracture parameters in addition to total fracture energies and maximum critical loads. The dynamic stress intensity factor $K_{Id}$ was computed for varying amounts of rubber contents from the obtained maximum critical loads and also toughening effects were investigated as well. The fracture surfaces produced under low velocity impact fur PVC/MBS composites were investigated by SEM. The results show that MBS rubber is very effective reinforcement material for toughening PVC.C.

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접착이음의 계면균열에 대한 파괴인성 및 평가방법 (Mehods of Fracture Toughness and Evaluation for Interface Crack in Adhesively Bonded Joints)

  • 정남용
    • 한국공작기계학회:학술대회논문집
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    • 한국공작기계학회 1998년도 춘계학술대회 논문집
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    • pp.220-226
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    • 1998
  • In this pater, a method of strength evaluation applying fracture mechanics in adhesively bonded joints of A1/A1 materials was investigated. Various adhesively bonded joints of double-cantilever beam with a interfacial crack in its adhesive layer were prepared for the fracture toughness test of comprehensive mixed mode conditions from nearly pure mode I to mode II. The experiment of fracture toughness was carried out under various mixed mode conditions with an interfacial crack and critical energy release rate, Gc by the experimental measurements of compliances was determined. From the results, fracture toughness on mixed mode with an interfacial crack is well characterized by strain energy release rate and a method of strength evaluation by the fracture toughness in adhesively bonded joints of A1/A1 materials was discussed.

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인장하중방향 변화를 받는 의사등방성 복합재 적층판의 피로손상 (Fatigue Damage of Quasi-Isotropic Composite Laminates Under Tensile Loading in Different Directions)

  • 김택현
    • 한국생산제조학회지
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    • 제8권2호
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    • pp.80-85
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    • 1999
  • The purpose of this work is to investigate fatigue damage of quasi-isotropic laminates under tensile loading in different directions. Low cycle fatigue tests of [0/-60/+60]a laminates and [+30/-30/90]s lamina tes were carried out. Material systems used are AS4/Epoxy and AS4/PEEK. The fatigue damage of [+30/-30/90]s is very different from that of [0/-60/+60]s. The position of delamination generated at AS4/Epoxy and AS$/PEEK laminates were differentiated by the matrix difference that is, we suppose, the value of both GIcr(critical energy release rate of mode-I) and GIIIcr(critical energy release rate of mode-III) difference.

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이방성재료 접합 띠판에 대한 면외 동적계면균열 (Mode III Dynamic Interfacial Crack in Bonded Anisotropic Strip Under Anti-Plane Deformation)

  • 박재완;최성렬
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 추계학술대회논문집A
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    • pp.111-116
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    • 2000
  • A semi-infinite interfacial crack propagated with constant velocity in two bonded anisotropic strip under out-of-plane clamped displacements is analyzed. The asymptotic stress and displacement fields near the crack tip are obtained, where the results get more general expressions applicable not only to isotropic/orthotropic materials but also to the extent of the anisotropic material having one plane of elastic symmetry for the interfacial crack. The dynamic stress intensity factor is obtained as a closed form, which is decreased as the velocity of crack propagation increases. The critical velocity where the stress intensity factor comes to zero is obtained, which agrees with the lower value between the critical values of parallel crack merged in the material 1 and 2 adjacent to the interface. The dynamic energy release rate is also obtained as a form related to the stress intensity factor.

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