• 제목/요약/키워드: fracture energy rate

검색결과 313건 처리시간 0.026초

폭발하중을 받는 콘크리트 보의 요소의존성 최소화 인장기준식 (A Tensile Criterion to Minimize FE Mesh-Dependency in Concrete Beam under Blast Loading)

  • 곽효경;강한글
    • 한국전산구조공학회논문집
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    • 제30권2호
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    • pp.137-143
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    • 2017
  • 본 논문에서는 파괴에너지이론에 기초하여 요소의존성을 최소화할 수 있는 인장파괴기준식을 제안하고 HJC(holmquist johnson cook), CSC(continuous surface cap), Orthotropic 모델을 이용한 폭발수치해석을 통해 기준식을 검증하였다. 폭발하중으로 인한 RC 보의 시간에 따른 중앙지점의 처짐을 실험결과와 비교하였다. 그 결과 기준식을 통해 산정된 파괴변형률을 수치해석상에 적용해줌으로써 해석결과의 요소의존성이 감소하였고 해의 정확성 또한 향상되는 것을 파악할 수 있었다.

국산 원자로용기 재료의 피로 및 파괴특성 연구 (A study on the fatigue and fracture characteristics of localized nuclear reactor vessel material)

  • 정순억
    • 대한기계학회논문집A
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    • 제21권10호
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    • pp.1626-1635
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    • 1997
  • It is important to ensure the reliability of the first localized reactor vessel steel. To satisfy with this purpose, a study on the impact/hardness, low cycle fatigue(LCF), crack growth rate(da/dN) and fracture toughness( ) of base material(BM) and weld metal(WM) were performed under room temperature air and corrosion conditions. A summary of the results is as folows : (1) Charpy impact absorbed energy of BM was the highest value, heat affected zoon(HAZ) and the lowest, WM. The hardness of BM was similar to HAZ. (2) Coefficients of Manson equation using the monotonic tensile test data were obtained for the present material. (3) The effects of stress ratio and ambient (120.deg. C and NaCl) condition on da/dN were investigated, da/dN with NaCl condition expressed the highest value. (4) The results of Charpy V-notch impact test had good correlation with $K_{IC}$ characteristics and the lowest curve of $K_{IC}$ for BM was derived, more researches about WM and HAZ are required hereafter.

탄성정수 및 입사파형의 변화에 따른 암반 내 균열전파양상에 관한 수치해석적 연구

  • 박승환;조상호
    • 한국지구물리탐사학회:학술대회논문집
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    • 한국지구물리탐사학회 2009년도 학술대회 초록집
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    • pp.155-159
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    • 2009
  • 화약류를 이용한 균열제어공법은 자원 및 석유개발, 토목 등 다양한 분야에서 적용되어 오고 있다. 암반을 대상으로 균열제어설계를 위해서는 다양한 암반의 물성과 가압방식의 변화에 따른 파괴과정을 이해할 필요가 있다. 본 연구에서는 반무한 암반 내 시추된 원형공벽에 임의의 입사파가 작용하여 주변에 균열이 전파하는 동적파괴현상을 수치해석적으로 모사하였다. 탄성정수는 국내의 암반분류에서 적용하는 물성치를 사용하였으며 하중가압속도는 1-100MPa/${\mu}s$의 범위까지 변화시키며 암반 내 균열전파양상을 살펴보았다.

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Crack Layer 이론을 이용한 배관용 고밀도 폴리에틸렌의 응력부식균열 진전 및 수명 예측 모델 (Modeling of stress corrosion crack growth and lifetime of pipe grade high density polyethylene by using crack layer theory)

  • 위정욱;최병호
    • 한국압력기기공학회 논문집
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    • 제11권2호
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    • pp.45-50
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    • 2015
  • In many cases, the field fracture mechanism of the thermoplastic pipe is considered as either brittle or environmental fractures. Thus the estimation of the lifetime by modeling slow crack growth considering such fracture mechanisms is required. In comparison of the some conventional and empirical equations to explain the slow crack growth rate such as the Paris' law, the crack layer theory can be used to simulate the crack and process zone growth behaviors precisely, so the lifetime of thermoplastic pipe can also be accurately estimated. In this study, the modified crack layer theory for the stress corrosion cracking (SCC) of high density polyethylene is introduced with detailed algorithm. The oxidation induction time of the HDPE is also considered for the reduction of specific fracture energy during exposed to chemical environments. Furthermore, the parametric study for an important SCC parameter is conducted to understand the slow crack growth behavior of SCC.

Mechanical Behaviors of CFRP Laminate Composites Reinforced with Aluminum Oxide Powder

  • Kwon, Oh-Heon;Yun, Yu-Seong;Ryu, Yeong-Rok
    • 동력기계공학회지
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    • 제18권6호
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    • pp.166-173
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    • 2014
  • In this study, a laminated composite material with dispersing aluminum oxide powder between the CFRP laminate plies, and also CFRP composites without aluminium oxide powder were fabricated for Mode I experiments using the DCB specimen and a tensile test. The behavior of the crack and the change of the interfacial fracture toughness were evaluated. Also in order to evaluate the damage mechanism for the crack extension, the AE sensor on the surface of the DCB test specimen was attached. AE amplitude was estimated for CFRP-alumina and CFRP composite. And the fracture toughness was evaluated by the stress intensity factor and energy release rate. The results showed that an unstable crack was propagated rapidly in CFRP composite specimen along with the interface, but crack propagation in CFRP-alumina specimen was relatively stable. From results, we show that aluminium oxide powder spreaded uniformly in the interface of the CFRP laminate carried out the role for preventing the sudden crack growth.

찢김 하중에서 단일 재료 및 이종 접합 재료에 따른 이중외팔보 시험편의 접착제 파손 특성 (Adhesive Fracture Characteristic of DCB Specimen due to Single and Heterogeneous Materials under Tearing Load)

  • 김재원;조재웅
    • 한국기계가공학회지
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    • 제20권4호
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    • pp.127-134
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    • 2021
  • In this study, the adhesive fracturing characteristics of a DCB specimen due to single and heterogeneous bonding materials under tearing load was investigated. The experiments were conducted to examine the fracturing properties of the adhesive DCB specimen. As an experimental condition, a forced displacement of 3mm/min was applied to one side while the other side was fixed. As a result of the experiment, it was found that the AL6061-T6 material was superior to the CFRP material in terms of maximum stress, specific strength, and energy release rate when compared to the adhesive fracturing property of a single material. We tested CFRP-AL, a heterogeneous bonding material, and compared its experimental results to the results from the single materials. Based on these results, CFRP-AL with a heterogeneous bonding material was observed to have the superior structural safety compared to single materials for the mode III fracture type.

Suppression of interfacial crack for foam core sandwich panel with crack arrester

  • Hirose, Y.;Hojo, M.;Fujiyoshi, A.;Matsubara, G.
    • Advanced Composite Materials
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    • 제16권1호
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    • pp.11-30
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    • 2007
  • Since delamination often propagates at the interfacial layer between a surface skin and a foam core, a crack arrester is proposed for the suppression of the delamination. The arrester has a semi-cylindrical shape and is arranged in the foam core and is attached to the surface skin. Here, energy release rates and complex stress intensity factors are calculated using finite element analysis. Effects of the arrester size and its elastic moduli on the crack suppressing capability are investigated. Considerable reductions of the energy release rates at the crack tip are achieved as the crack tip approached the leading edge of the crack arrester. Thus, this new concept of a crack arrester may become a promising device to suppress crack initiation and propagation of the foam core sandwich panels.

텅스텐 중합금 복합관통자 제조 (Manufacturing of Tungsten Heavy Alloy Composites for Kinetic Energy Penetrator)

  • 송흥섭;김은표;박경진;류주하
    • 한국분말재료학회지
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    • 제11권5호
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    • pp.369-375
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    • 2004
  • A new concept of tungsten heavy alloy composite was suggested and manufactured in this study for the kinetic energy penetrator. The composite heavy alloy was composed of two parts, the center was molybdenum added heavy alloy compositions which were designed to promote the self-sharpening effect and outside was conventional heavy alloy in order to sustain the severe stress condition in the muzzle during the firing. The center part showed an intergranular and brittle mode at tungsten/tungsten interfaces by which self-sharpening effect could be activated. On the other hand, that of outside showed conventional ductile fracture mode under high strain rate condition. From the sub-scale penetration test, the depth of penetration in heavy alloy composites showed greater values than those of conventional tungsten heavy alloys. It is suggested that the heavy alloy composite could be considered as one of the future penetrator materials.

Interlaminar stresses and delamination of composite laminates under extension and bending

  • Nguyen, Tien Duong;Nguyen, Dang Hung
    • Structural Engineering and Mechanics
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    • 제25권6호
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    • pp.733-751
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    • 2007
  • The metis element method (Hung 1978) has been applied to analyse free edge interlaminar stresses and delamination in composite laminates, which are subjected to extension and bending. The paper recalls Lekhnitskii's solution for generalized plane strain state of composite laminate and Wang's singular solution for determination of stress singularity order and of eigen coefficients $C_m$ for delamination problem. Then the formulae of metis displacement finite element in two-dimensional problem are established. Computation of the stress intensity factors and the energy release rates are presented in details. The energy release rate, G, is computed by Irwin's virtual crack technique using metis elements. Finally, results of interlaminar stresses, the three stress intensity factors and the energy release rates for delamination crack in composite laminates under extension and bending are illustrated and compared with the literature to demonstrate the efficiency of the present method.

직교 이방성체의 동적 응력확대계수에 관한 연구(I) (A Study on the Dynamic Stress Intensity Factor of Orthotropic Materials(I))

  • 이광호;황재석;최선호
    • 대한기계학회논문집
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    • 제17권2호
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    • pp.313-330
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    • 1993
  • The propagating crack problems under dynamic plane mode in orthotropic material is studied in this paper. To analyze the dynamic fracture problems in orthortropic material, it is important to know the dynamic stress components and dynamic displacement components around the crack tip. Therefore the dynamic stress components of dynamic stress field and dynamic displacement components of dynamic displacement field in the crack tip of orthotropic material under the dynamic load and the steady state in crack propagation were derived. When the crack propagation speed approachs to zero, the dynamic stress component and dynamic displacement components derived in this study are identical to the those of static state. In addition, the relationships between dynamic stress intensity factor and dynamic energy release rate are determinded by using the concept of crack closure closure energy with the dynamic stresses and represented according to physical properties of the orthotrophic material and crack speeds. The faster the crack velocity, the greater the stress value of stress components in crack tip. The stress value of the stress component of crack tip is greater when fiber direction coincides with the crack propagation than when fider direction is normal to the crack propagation.