NASA NTRS ยท 19730003200
Buckling of circular cylindrical shells under dynamically applied axial loads
Abstract
A theoretical and experimental study was made of the buckling characteristics of perfect and imperfect circular cylindrical shells subjected to dynamic axial loading. Experimental data included dynamic buckling loads (124 data points), high speed photographs of buckling mode shapes and observations of the dynamic stability of shells subjected to rapidly applied sub-critical loads. A mathematical model was developed to describe the dynamic behavior of perfect and imperfect shells. This model was based on the Donnell-Von Karman compatibility and equilibrium equations and had a wall deflection function incorporating five separate modes of deflection. Close agreement between theory and experiment was found for both dynamic buckling strength and buckling mode shapes.
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Tulk, J. D.. 1972-06-01. Buckling of circular cylindrical shells under dynamically applied axial loads. https://ntrs.nasa.gov/citations/19730003200
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