J. Herencia
This work presents a semi-analytical approach to calculate rapidly but accurately the buckling onset of metallic and composite circular cylindrical shells with various boundary conditions under in-plane and/or pressure loads by the Rayleigh-Ritz method. Results are compared with analytical solutions and detailed finite element models reported in the literature. The proposed approach allows a quick buckling analysis of circular cylindrical shells, which makes it an ideal candidate to be used as part of an optimization scheme and/or to reduce potentially the number of detailed finite element models employed in the early design phases.
Keywords:
You do not have permission to edit this page, for the following reason:
You are not allowed to execute the action you have requested.
You can view and copy the source of this page.
Return to Herencia 2023a.
Accepted on 05/12/23Submitted on 31/05/23
Licence: Other
Views 0Recommendations 0