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Information Journal Paper

Title

ANALYSIS OF EFFECTIVE PARAMETERS ON THE BUCKLING OF GRID STIFFENED COMPOSITE SHELLS BASED ON FIRST ORDER SHEAR DEFORMATION THEORY

Pages

  51-61

Abstract

GRID STIFFENED COMPOSITE SHELLS are one of the most important structures in aerospace industries. In this study critical buckling load of these structures with diamond shape stiffeners under axial loading based on SMEARED METHOD is presented. The effect of shell thickness, angle of fibers in shell and the direction of stiffeners into the buckling load is determined. First-order shear deformation theory based upon the RITZ METHOD is used to calculation of critical buckling load of these structures. In the use of FSDT theory, transverse shear forces in stiffeners have been considered. The results are compared with FEM solution with clamped boundary condition.

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    APA: Copy

    YAZDANI, M., GHASEMI, M.A., & HOSEINI, S.M.. (2013). ANALYSIS OF EFFECTIVE PARAMETERS ON THE BUCKLING OF GRID STIFFENED COMPOSITE SHELLS BASED ON FIRST ORDER SHEAR DEFORMATION THEORY. MODARES MECHANICAL ENGINEERING, 13(10), 51-61. SID. https://sid.ir/paper/177803/en

    Vancouver: Copy

    YAZDANI M., GHASEMI M.A., HOSEINI S.M.. ANALYSIS OF EFFECTIVE PARAMETERS ON THE BUCKLING OF GRID STIFFENED COMPOSITE SHELLS BASED ON FIRST ORDER SHEAR DEFORMATION THEORY. MODARES MECHANICAL ENGINEERING[Internet]. 2013;13(10):51-61. Available from: https://sid.ir/paper/177803/en

    IEEE: Copy

    M. YAZDANI, M.A. GHASEMI, and S.M. HOSEINI, “ANALYSIS OF EFFECTIVE PARAMETERS ON THE BUCKLING OF GRID STIFFENED COMPOSITE SHELLS BASED ON FIRST ORDER SHEAR DEFORMATION THEORY,” MODARES MECHANICAL ENGINEERING, vol. 13, no. 10, pp. 51–61, 2013, [Online]. Available: https://sid.ir/paper/177803/en

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