• 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.

• 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.

• 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.

• 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.

• 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.

• 소성∙가공
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• 제11권8호
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• pp.682-690
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• 2002

The formation of adiabatic shearband in tungsten heavy alloys(WHA) was studied in this investigation. Five prismatic specimens were loaded by high velocity impacts and treated as plane strain problems. To find out the effect of particle's volume ratio, specimens containing 81%, 93% and 97% volume percents of tungsten particles were used. Also the effects of particle's geometry and size on the formation of shearband were studied for 81% volume percent alloys by small size particle model, large size particle model and undulated particle models, and the results were discussed.be used to diagnose the causes of necking and fracture in industrial practice and to investigate whether these defects were caused by material property variation, changes in lubrication, or incorrect press settings. In non-axisymmetric deep drawing, three modes of forming regimes are found: draw, stretch, plane strain. The stretch mode for non-axisymmetric deep drawing could be defined when the major and minor strains are positive. The draw mode could be defined when the major strain is positive and minor strain is negative, and plane strain mode could be defined when the major strain is positive and minor strain is zero. Through experiments the draw mode was shown on the wall and flange are one of a drawn cup, while the plane strain and the stretch mode were on the punch head and the punch corner area respectively, We observed that the punch load of elliptical deep drawing was decreased according to increase of die corner radius and the thickness deformation of minor side was more large than major side.