Investigation of the Effective Parameters on Buckling Load of FML Cylindrical Panel Using FSDT Shells Theory

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Abstract:
In this paper, the buckling load and buckling modes of FML panel, using first order shear deformation theory, has been studied, based on the Reddy's numerical solution. Because of various applications of FML shells, GLARE panel was considered. The effects of geometry, lay-up, and MVF were determined. Boundary conditions were simply supported and the panel was axially loaded. The results for Glare panel are presented and discussed. Reducing the number of metal layers at a constant MVF increases the Buckling load. The results from the finite element model were found to be in general agreements with the other references.
Language:
Persian
Published:
Aerospace Mechanics Journal, Volume:6 Issue: 4, 2011
Page:
95
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سامانه نویسندگان
  • Ali Mozaffari
    Corresponding Author (1)
    (1378) دکتری هوافضا، MAI, RUSSIA
    Mozaffari، Ali
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