PG-EAM - Graduate Program in Aeronautical and Mechanical Engineering
PT EN
Article 2000

Buckling optimization of composite axisymmetric cylindrical shells under uncertain loading combinations

Authors

Hansen, Jorn S.

Collection of Technical Papers AIAA ASME ASCE AHS ASC Structures Structural Dynamics and Materials Conference , vol. 1 , no. I , pp. 112-122

ISSN: 02734508

2
Citations
2
Authors

Abstract

Optimal elastic buckling loads of composite axisymmetric circular cylinders under uncertain loading conditions are investigated. The mechanical loads applied to the cylinder are a combination of axial compression, lateral pressure and torsion. Additionally, these loads are allowed to vary within a certain class of admissible loads during the optimization search, as opposed to the restriction of fixed loads in the traditional optimization. The consideration of a degree of uncertainty in the mechanical loads leads to optimal designs which are inherently insensitive to perturbations and/or randomness in the applied loads.

Architecture (ENGI) Materials Science (all) (MATE) Aerospace Engineering (ENGI) Mechanics of Materials (ENGI) Mechanical Engineering (ENGI)
: Scopus
Last Update: 2026-06-25
: 2-s2.0-0033666178