مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

video

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

sound

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Persian Version

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

View:

340
مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Download:

145
مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Cites:

Information Journal Paper

Title

NONLINEAR DEFORMATION ANALYSIS AND MODELING OF COMPOSITE WITH ALUMINUM LAYERS

Pages

  39-45

Abstract

 Fiber metal laminates (FMLs) are new composite materials consisting of thin metal layers and high strength composite layers. ARALL (Aramid aluminum laminate) is a family of the FML that consists of thin aluminum sheets along with Kevlar/epoxy composite layers. This material has many advantages such as light weight, excellent corrosion, fatigue and impact resistance. Since, ARALL is a new material, therefore presentation of a model for nonlinear behavior analysis is important. This paper presents the ELASTIC– PLASTIC behavior of ARALL under inplane tensile loading. For this purpose, the ORTHOTROPIC PLASTICITY theory and modified classical laminated plate theory are used. In the ORTHOTROPIC PLASTICITY model, a three parameter plastic potential function is used. In the second theory, the Kevlar/epoxy composite layers and aluminum sheets are assumed to be linearly elastic and orthotropic ELASTIC– PLASTIC solids, respectively. Good agreement is obtained between results of two models. The results show that the case study behavior is almost BILINEAR under tensile loading and it has more strength in longitudinal direction in comparison to transverse direction. Variation of the POISSON’S RATIO is considered in longitudinal and transverse loading too.

Cites

  • No record.
  • References

    Cite

    APA: Copy

    ESFANDIAR, HABIB, ADIB NAZARI, SAEED, MONFARED, VAHID, & KHATIB, ALI. (2010). NONLINEAR DEFORMATION ANALYSIS AND MODELING OF COMPOSITE WITH ALUMINUM LAYERS. JOURNAL OF MECHANICAL RESEARCH AND APPLICATION (JMRA), 2(1), 39-45. SID. https://sid.ir/paper/579917/en

    Vancouver: Copy

    ESFANDIAR HABIB, ADIB NAZARI SAEED, MONFARED VAHID, KHATIB ALI. NONLINEAR DEFORMATION ANALYSIS AND MODELING OF COMPOSITE WITH ALUMINUM LAYERS. JOURNAL OF MECHANICAL RESEARCH AND APPLICATION (JMRA)[Internet]. 2010;2(1):39-45. Available from: https://sid.ir/paper/579917/en

    IEEE: Copy

    HABIB ESFANDIAR, SAEED ADIB NAZARI, VAHID MONFARED, and ALI KHATIB, “NONLINEAR DEFORMATION ANALYSIS AND MODELING OF COMPOSITE WITH ALUMINUM LAYERS,” JOURNAL OF MECHANICAL RESEARCH AND APPLICATION (JMRA), vol. 2, no. 1, pp. 39–45, 2010, [Online]. Available: https://sid.ir/paper/579917/en

    Related Journal Papers

  • No record.
  • Related Seminar Papers

  • No record.
  • Related Plans

  • No record.
  • Recommended Workshops






    Move to top
    telegram sharing button
    whatsapp sharing button
    linkedin sharing button
    twitter sharing button
    email sharing button
    email sharing button
    email sharing button
    sharethis sharing button