What is it about?
An analytical solution predicts critical buckling loads for doubly-curved laminates under compression, shear, and bending, aligning well with finite element analysis results, offering comprehensive insight into buckling behavior for improved aerospace structural design.
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Why is it important?
The study highlights the significance of developing an analytical solution for predicting critical buckling loads in curved laminates for aerospace structures. It underscores the vulnerability of curved panels to buckling and the adverse effects on aircraft performance. The paragraph emphasizes the limitations of past research, which mainly focused on flat panels or simplified analyses, and the need for a comprehensive solution to address a wider range of scenarios.
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This page is a summary of: An analytical solution to estimate the critical buckling load of doubly-curved laminates under a combined load of uni-axial compression, in-plane shear and bending moment, Mechanics Based Design of Structures and Machines, May 2022, Taylor & Francis,
DOI: 10.1080/15397734.2022.2081977.
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