• 제목/요약/키워드: adiabatic shear band

검색결과 19건 처리시간 0.019초

4340강의 단열 전단밴드생성에 대한 유한요소해석 및 실험적 고찰 (Finite element analysis and experiment on the formation of adiabatic shear band in 4340 steel)

  • 정동택;유요한
    • 대한기계학회논문집
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    • 제18권5호
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    • pp.1134-1143
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    • 1994
  • A study of adiabatic shear band formation and propagation of 4340 steel was done using the stepped speciment which was subjected to high velocity impact. The high velocity impact was performed on compression Hopkinson bar impact machine. After the controlled impact, the specimen was prepared for visual inspection. Numerical simulation was also performed with same geometrical dimension using explicit time integration finite element code. Experimental results were then compared with the numerical prediction. It was found that the numerical prediction is quite accurate, average thickness of adiabatic shear band is about $10{\mu}m$, the macro crack around shoulder is due to folding, and the deformation control ring is effective to freeze the propagation of adiabatic shear band.

계단시편의 간극이 단열전단밴드의 형성에 미치는 영향 (Effects of Clearance on the Formation of Adiabatic Shear Band in Stepped Specimen)

  • 유요한;전기영;정동택
    • 대한기계학회논문집
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    • 제17권7호
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    • pp.1700-1709
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    • 1993
  • The stepped specimen which is subjected to step loading is modeled to study the initiation and growth of adiabatic shear band using explicit time integration finite element method. Three different clearance sizes are tested. The material model for the stepped specimen includes effects of strain hardening, strain rate hardening and thermal softening. It is found that the material inside the fully grown adiabatic shear band experiences three phase of deformation, (1) homogeneous deformation phase, (2) initiation/incubation phase, and (3) fast growth phase. The second phase of deformation is initiated after sudden shear stress drop which occurs at the same time regardless of the clearance size. The incubation time prior to fast growth phase increases, as the clearance size of the stepped specimen increases. Whereas, after incubation period, the growth rate of the adiabatic shear band decreases, as the clearance size decreases. It is also found that two adiabatic shear band may develop instead of one for the smaller clearance size.

텅스텐 중합금의 단열전단밴드 형성 연구 (A study on the Formation of Adiabatic Shear Band of Tungsten Heavy Alloys)

  • 이승우;문갑태;홍성인
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 2002년도 춘계학술대회 논문집
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    • pp.187-190
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    • 2002
  • To study adiabatic shear band formation of tungsten heavy alloys, 5 prismatic specimens are loaded by high velocity impacts and treated as plane strain problems. Their volume percent of tungsten particles in WHA are 81%, 93% and 97% respectively and for the fixed 81% volume percent, small size particle model, large size particle model, undulated particle models are considered and then, the effects of particle's volume ratio, geometry and size to the formation of shear band are discussed.

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단열 전단 밴드의 유한요소 해석 (Finite Element Anmllysis of Adiabatic Shear Band)

  • 유요한;전기영;정동택
    • 대한기계학회논문집
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    • 제16권8호
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    • pp.1519-1529
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    • 1992
  • 본 연구에서는 단열 전단 밴드의 특성 규명을 위하여 특별히 고안된 계단 형 상 시편(stepped specimen)의 수치해석을 통하여 단열 전단 밴드의 형성과 성장(init- iation and growth of adiabatic shear band)에 관한 체계적 해석을 시도해 보았다. 금번 논문에서는 우선 격자 크기(mesh size)와 충격 속도(impact velocity)가 단열 전 단 밴드의 형성 및 성장에 미치는 영향과 제반 특성을 규명할 계획이며 차후 재료의 기하학적 형상 등이 단열 전단 밴드의 형성 및 성장에 미치는 영향에 대해서도 단계적 연구를 시도할 계획이다. 해석을 위하여 가공경화효과, 변형률 속도 경화효과(stra- in rate hardening effect), 열적연화효과 등을 고려할 수 있는 구성 방정식(constit- utive equation)을 갖춘 엑스플리시트 시간적분 유한요소 코드(explicit time integr- ation finite element code)를 사용하였으며 기존의 연구 결과와는 달리 어떠한 인위 적 결함도 해석에 사용하지 않았다.

고속 절삭공정 중 톱니형 칩 생성 예측 (Prediction of Serrated Chip Formation in High Speed Metal Cutting)

  • 임성한;오수익
    • 소성∙가공
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    • 제12권4호
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    • pp.358-363
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    • 2003
  • Adiabatic shear bands have been observed in the serrated chip during high strain rate metal cutting process of medium carbon steel and titanium alloy The recent microscopic observations have shown that dynamic recrystallization occurs in the narrow adiabatic shear bands. However the conventional flow stress models such as the Zerilli-Armstrong model and the Johnson-Cook model, in general, do not predict the occurrence of dynamic recrystallization (DRX) in the shear bands and the thermal softening effects accompanied by DRX. In the present study, a strain hardening and thermal softening model is proposed to predict the adiabatic shear localized chip formation. The finite element analysis (FEA) with this proposed flow stress model shows that the temperature of the shear band during cutting process rises above 0.5Τ$_{m}$. The simulation shows that temperature rises to initiate dynamic recrystallization, dynamic recrystallization lowers the flow stress, and that adiabatic shear localized band and the serrated chip are formed. FEA is also used to predict and compare chip formations of two flow stress models in orthogonal metal cutting with AISI 1045. The predictions of the FEA agreed well with the experimental measurements.s.

미소 전단 띠 형성에 의한 톱니형 칩 생성 예측 (Prediction of Serrated Chip Formation due to Micro Shear Band in Metal)

  • 임성한;오수익
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 2003년도 춘계학술대회논문집
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    • pp.427-733
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    • 2003
  • Adiabatic shear bands have been observed in the serrated chip during high strain rate metal cutting process of medium carbon steel and titanium alloy. The recent microscopic observations have shown that dynamic recrystallization occurs in the narrow adiabatic shear bands. However the conventional flow stress models such as the Zerilli-Armstrong model and the Johnson-Cook model, in general, do not predict the occurrence of dynamic recrystallization (DRX) in the shear bands and the thermal softening effects accompanied by DRX. In the present study, a strain hardening and thermal softening model is proposed to predict the adiabatic shear localized chip formation. The finite element analysis (FEA) with this proposed flow stress model shows that the temperature of the shear band during cutting process rises above 0.5T$\sub$m/. The simulation shows that temperature rises to initiate dynamic recrystallization, dynamic recrystallization lowers the flow stress, and that adiabatic shear localized band and the serrated chip are formed. FEA is also used to predict and compare chip formations of two flow stress models in orthogonal metal cutting with AISI 1045. The predictions of the FEA agreed well with the experimental measurements.

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단열전단변형에서 국부화에 대한 수치해석적 연구 (A Study of Localization of the Adiabatic Shear Band with Numerical Method)

  • 이병섭
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 1999년도 춘계학술대회논문집
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    • pp.225-228
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    • 1999
  • In a plastically deformed body the formation of a shear band is widely observed in the engineering materials during rapidly forming process for a thermally rate-sensitive material. The localized shear bond stems from evolution of a narrow region in which intensive plastic flow occurs. The shear band often plays as a precursor of the ductile fracture during a forming process. The objectives of this study are to investigate the localization behaivor by using numerical method thus predict the failure. In this work the implicit finite difference scheme is preformed due to the ease of covergence and the numerical stability. This study is based on an analysised material with hardening as well as thermally softening behavior which includes isotropy strain hardening. Furthermore this paper suggests that an anticipated and suggested a kinematic hardening constitutive equation be requried to predicte a more accurate strain level wherein a shear band occurs.

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텅스텐 중합금의 단열전단밴드 형성 및 국부화에 대한 연구 (A Study of Localization for Adiabatic Shear Band in WHA(Tungsten Heavy Alloy))

  • 황두순;홍성인
    • 한국추진공학회지
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    • 제11권6호
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    • pp.18-25
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    • 2007
  • 열적으로 민감한 재료의 소성 변형에 있어서, 전단력에 의한 전단밴드(shear band)는 많은 공학적인 재료에서 관찰되고 있으며 전단밴드의 형성이 가속화됨에 따라 밴드의 변화량이 많고 폭이 좁은 국부화(localization) 현상이 발생하게 되는데, 이는 가공물에 치명적인 파단을 가져올 수 있는 현상이다. 본 연구에서는 텅스텐 중합금(tungsten heavy alloy, WHA)의 관통 메커니즘을 분석하기 위해 높은 변형률의 조건하에서 관찰될 수 있는 전단밴드(shear band)의 형성과 국부화 현상에 대하여 열적 조건을 고려하여, 고속변형률에서 다결정 금속의 전단밴드 구성에 기초를 둔 메커니즘을 수치적으로 연구하였다.

재료의 특징에 따른 국부화에 대한 수치해석적 연구 (A Study of Localization with Material Properties Using Numerical Method)

  • 황두순;이병섭;이용성;윤수진;홍성인
    • 소성∙가공
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    • 제9권4호
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    • pp.395-403
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    • 2000
  • Formation of Shear Band under the adiabatic condition is widely observed In the engineering materials during rapidly forming process lot a thermally rate-dependent material. The shear band stems from evolution of a narrow region in which an intensive plastic flow occurs. The shear band often plays a role of a precursor of the ductile fracture during a forming process. The objective of this study is to investigate the localization behavior using numerical method. In this work, the implicit finite difference scheme is employed due to the ease of convergence and the numerical stability It is noted that physical and mechanical properties of materials determine how the shear band is formed and then localized. Material properties can be characterized with inertia number dissipation number and diffusion number. It is observed that the dimensionless numbers effect on localization. Using a parametric study, comparison was made between CRS-1018 steel with WHA (tungsten heavy alloy). The deformation behavior of material in this study include an isotropic hardening as well as thermal softening. Moreover, this study suggests that a kinematic hardening constitutive relation be required to predict a more accurate strain level at a shear band.

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Non-local 이론을 적용한 단열전단밴드의 국부화에 대한 연구 (A Study of Localization for Adiabatic Shear Band Using Non-local Theory)

  • 이용성;이병섭;황두순;윤수진;홍성인
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 2001년도 춘계학술대회 논문집
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    • pp.205-208
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    • 2001
  • Localized shear band is investigated through the analysis of one-dimensional model for simple shearing deformation of thermally rate dependent material. Generally mesh size or interval of nodes play an important role in determining the overall flow behavior of the material. In order to observe these size effects we adapted non-local theory by including higher order strain gradients of the equivalent strain into the constitutive equation for the flow stress. for the ease of convergence and numerical stability the inplicit finite difference scheme is employed.

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