Accession Number : AD0862102
Title : The Maximum Strength of Initially Imperfect, Axially Compressed, Circular Cylindrical Shells.
Descriptive Note : Final rept.,
Corporate Author : STANFORD UNIV CA DEPT OF AERONAUTICS AND ASTRONAUTICS
Personal Author(s) : Mayers, Jean ; Wesenberg, Donald L.
Report Date : AUG 1969
Pagination or Media Count : 68
Abstract : The maximum strength of initially imperfect, axially compressed, circular cylindrical shells has been studied with the use of Reissner's variational principle, von Karman-Donnell shell theory, and a deformation theory of plasticity. The results of the present analysis reflect families of load-end shortening curves for long circular cylinders. For a given material, each curve relates not only to an imperfection parameter which provides a loading path into the inelastic range but also to the radius-to-wall thickness ratio. Significant maximum strength reductions are obtained, relative to predictions based on linear-elastic theory, for specific materials in the range of radius-to-thickness ratios of practical interest. (Author)
Descriptors : (*CYLINDRICAL BODIES, SHELLS(STRUCTURAL FORMS)), (*SHELLS(STRUCTURAL FORMS), FAILURE(MECHANICS)), LOADS(FORCES), COMPRESSIVE PROPERTIES, BUCKLING, DEFORMATION, ELASTIC SHELLS, PLASTIC PROPERTIES, STRESSES, STRAIN(MECHANICS), GRAPHICS, ANALOG SYSTEMS, CALCULUS OF VARIATIONS, NICKEL, COPPER, ALUMINUM ALLOYS, ELECTROFORMING.
Subject Categories : Structural Engineering and Building Technology
Distribution Statement : APPROVED FOR PUBLIC RELEASE