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Buckling of circular cylindrical shells under dynamically applied axial loadsA 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.
Document ID
19730003200
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Tulk, J. D.
(Toronto Univ. Ontario)
Date Acquired
September 2, 2013
Publication Date
June 1, 1972
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-129086
UTIAS-160
Report Number: NASA-CR-129086
Report Number: UTIAS-160
Accession Number
73N11927
Funding Number(s)
CONTRACT_GRANT: NGR-52-026-011
CONTRACT_GRANT: NRC A-2783
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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