• 제목/요약/키워드: Adiabatic shearing

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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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금속 장갑재료의 개발기술 및 발전전망 (Technological Review on the Development of Metallic Armor Materials)

  • 김홍규;홍성석;심인옥
    • Composites Research
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    • 제24권2호
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    • pp.46-50
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    • 2011
  • 이 논문은 전투차량의 주 장갑재료로 사용되는 금속장갑재료의 개발현황 및 방탄성능에 영향을 미치는 조직학적 요인들을 중심으로 방탄성 향상을 위한 요소기술을 살펴보고, 향후 금속장갑재의 발전전망에 대하여 서술하였다. 금속장갑재는 요구되는 방호특성에 따라 사용되는 합금계가 다르지만 강도와 인성을 최적화하여 위협 탄에 대한 관통저항성 및 취성파단에 대한 저항성을 극대화하는 것이 필요하며, 이를 위해서는 금속재료의 방탄조건에서 특정적으로 나타나는 단열전단현상을 이해하고 적절히 제어하는 기술이 요구된다.

The Effect of In-flight Bulk Metallic Glass Particle Temperature on Impact Behavior and Crystallization

  • Kim, Soo-Ki;Yoon, Sang-Hoon;Lee, Chang-Hee
    • 한국분말야금학회:학술대회논문집
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    • 한국분말야금학회 2006년도 Extended Abstracts of 2006 POWDER METALLURGY World Congress Part 1
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    • pp.242-243
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    • 2006
  • NiTiZrSiSn bulk metallic glass powder was produced using inert gas atomization and then was sprayed onto a SS 41 mild steel substrate using the kinetic spraying process. Through this study, the effects of thermal energy of in-flight particle and crystallization degree by powder preheating temperature were evaluated. The deformation behavior of bulk metallic glass is very interesting and it is largely dependent on the temperature. The crystalline phase formation at impact interface was dependent on the in-flight particle temperature. In addition, variations in the impact behavior need to be considered at high strain rate and in-flight particle temperature.

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