Experimental investigation of the effect of general imperfections on the buckling of cylindrical shells

Imperfection survey data on cylindrical shells before and during axial compression loading up to buckling loa

A Multimode Analysis for Calculating Buckling Loads of Imperfect Cylindrical Shells

By expanding the response of a cylindrical shell in truncated Fourier series, the nonlinear Donnell type shell equations for imperfect stiffened shells were reduced to a set of linear equations in the correction terms by Newton's method of quasilinearization. Solutions were obtained for isotropic and for ring and stringer stiffened shells. The amplitudes of the initial imperfections used in the analysis were calculated from the corresponding Imbert-Donnell imperfection models. The free parameters in this imperfection model were obtained by least square fitting the harmonics of the experimentally measured initial imperfections. It was possible in all cases to achieve satisfactory correlation using only a few suitably chosen deflection and imperfection modes

User's guide for 'ANIPBIF' - Program to calculate the buckling load of axially compressed anisotropic shells with a single axisymmetric imperfection -

Aerospace Engineerin

Past, present and future of shell stability analysis

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User's guide for 'ANICBIF' - Program to calculate the buckling load of anisotropic shells under external pressure with a single axisymmetric imperfection -

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User's guide for 'ANCBFACT' - Program to calculate the buckling load of anisotropic shells under external pressure with a single asymmetric imperfection -

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