Journals / Turkish Journal of Engineering and Environmental Sciences / 2003 / Cilt: 27 - Sayı: 4

The Buckling of Laminated Cylindrical Thin Shells under Torsion Varying as a Linear Function of Time

Pages
237–245
DOI
—
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AI Summary & Key Takeaways

AI Insight
⚡ TL;DR(Too Long; Didn't Read)

Finally after performing the computations, the effects of the variations of the numbers and ordering of layers, loading speed, and the ratio of radius to thickness on the critical parameters are investigated.

📌 3 Key Takeaways

🎯
Objective & Hypothesis:The buckling of laminated orthotropic cylindrical thin shells under torsion, which is a linear function of time, has been investigated.
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Key Findings & Data:First, fundamental relations and the modified Donnell type stability equations of the laminated cylindrical thin shells are derived.
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Conclusion & Impact:Finally after performing the computations, the effects of the variations of the numbers and ordering of layers, loading speed, and the ratio of radius to thickness on the critical parameters are investigated.
🔬Design:Research Article
📍Scope:Comprehensive Sample
⚙️Variables:Buckling · Laminated · Orthotropic shell

Abstract

The buckling of laminated orthotropic cylindrical thin shells under torsion, which is a linear function of time, has been investigated. First, fundamental relations and the modified Donnell type stability equations of the laminated cylindrical thin shells are derived. Applying Galerkin's method, a differential equation having a variable coefficient depending on time is obtained and by applying the Ritz-type variational method to these equations, general formulas for static and dynamic critical loads, corresponding wave numbers and the dynamic factor are obtained. Finally after performing the computations, the effects of the variations of the numbers and ordering of layers, loading speed, and the ratio of radius to thickness on the critical parameters are investigated.

Özet

The buckling of laminated orthotropic cylindrical thin shells under torsion, which is a linear function of time, has been investigated. First, fundamental relations and the modified Donnell type stability equations of the laminated cylindrical thin shells are derived. Applying Galerkin's method, a differential equation having a variable coefficient depending on time is obtained and by applying the Ritz-type variational method to these equations, general formulas for static and dynamic critical loads, corresponding wave numbers and the dynamic factor are obtained. Finally after performing the computations, the effects of the variations of the numbers and ordering of layers, loading speed, and the ratio of radius to thickness on the critical parameters are investigated.

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Cite This Article

SOFIYEV, A. H., ZERİN, Z., TÜRKMEN, M. (2003). The Buckling of Laminated Cylindrical Thin Shells under Torsion Varying as a Linear Function of Time. Turkish Journal of Engineering and Environmental Sciences, Cilt: 27 - Sayı: 4, 237–245. https://ajindex.com/articles/369270

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