• Title/Summary/Keyword: induced anisotropy

Search Result 163, Processing Time 0.039 seconds

Finite Element Analysis for Forming Process of Polycrystalline Metal Including Texture Development (집합조직의 발전을 반영하는 다결정재의 성형공정해석)

  • 김응주;이용신
    • Proceedings of the Korean Society for Technology of Plasticity Conference
    • /
    • 1996.03a
    • /
    • pp.62-72
    • /
    • 1996
  • A process model is formulated considering the effect of crystallographic testure developed in forming process. The deformation induced plastic anisotropy can be predicted by capturing the evolution of texture during large deformatin in the poly crystaline aggregate. The anisotropic stiffness matrix for the aggregate is derived and implemented in Dulerian finite element code. As an application , the evolution of texture in rolling, drawing and extrusion processes are simulated . The numerical results show good agreement with reported experimental textures.

  • PDF

Finite Element Analysis for Steady State Forming Process of Polycrystalline Metal Including Texture Development (집합조직의 발전을 반영하는 다결정재의 정상상태성형공정해석)

  • 김응주;이용신
    • Transactions of Materials Processing
    • /
    • v.5 no.4
    • /
    • pp.297-304
    • /
    • 1996
  • A process model is formulated considering the effect of crystallographic texture developed in forming process. The deformation induced plastic anisotropy can be predicted by capturing the evolution of texture during large deformation in the polycrystalline aggregate. The anisotropic stiffness matrix for the aggregate is derived and implemented in Eulerian finite element code using a Consistent Penalty method. As an application the evolution of texture in rolling drawing and extrusion processes are simulated. The numerical results show good agreements with report-ed experimental textures.

  • PDF

Structural Modelling of Tapered Composite Aircraft Wings with Initial Angle of Attack using Thin-Walled Beam (얇은 벽 보를 이용한 초기 받음각이 있는 테이퍼형 복합재료 항공기 날개의 구조 모델링)

  • Kim, Keun-Taek;Song, Ohseop
    • Journal of Aerospace System Engineering
    • /
    • v.3 no.2
    • /
    • pp.1-11
    • /
    • 2009
  • A structural modelling for study on dynamic characteristics of tapered composite aircraft wings in the form of thin-walled beam is presented. The proposed structural model includes effects of transverse shear flexibility exhibited by the advanced composite materials and warping restraint characterizing elastic anisotropy and induced structural couplings. The complex effects of these factors could have a role in more efficient analysis on those structural models.

  • PDF

Photo-Alignment Using Polyimide Containing Methoxy Cinnamate Derivatives

  • Kim, Su-Young;Shin, Sung-Eui;Shin, Dong-Myung
    • 한국정보디스플레이학회:학술대회논문집
    • /
    • 2009.10a
    • /
    • pp.668-671
    • /
    • 2009
  • Photosensitive polyimide containing methoxy cinnamate derivatives as a photo-alignment layer is investigated. The anisotropy of alignment layer was induced by irradiation linearly polarized UV (LPUV). We studied the effect of the methoxy cinnamate groups on alignment LCs.

  • PDF

Microscale Analysis of the Anisotropic Sintering of Metal Powder Compacts

  • Vagnon, Alexandre;Kapelski, Georges;Bouvard, Didier.
    • Proceedings of the Korean Powder Metallurgy Institute Conference
    • /
    • 2006.09a
    • /
    • pp.260-261
    • /
    • 2006
  • The behaviour of steel powder compacts during sintering has been investigated by dilatometry and X-ray computed microtomography. Dilatometry measurements showed that the anisotropic deformation results from various phenomena arising at different moments of the cycle including the delubrication stage. Microtomography provided 3D images of the microstructure induced by prior die pressing and its changes throughout sintering. Finally a schematic description of the main phenomena responsible for the deformation of metal powder compacts during sintering is proposed.

  • PDF