A NUMERICAL ANALYSIS OF ELASTIC-PLASTIC THIN SHELLS OF REVOLUTION CONTAINING DISCONTINUITIES
Analysis of the common junction of three dissimilar general shells of revolution
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Analysis of the common junction of three dissimilar general shells of revolution
Elastic spheroidal shell of revolution under external pressure described by buckling and postbuckling theory
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Dynamic response of thin elastic conical shells subject to blast loading - membrane theory
Equations for thin elastic spherical shells and digital program for analysis of stresses and deformation of fixed edge segmental spherical shells - solution by finite difference technique
Tests were conducted to determine the elastic stability of large shell structures. The configuration of the shells and the instrumentation used in the measurements are described. The testing procedures are explained. Results of the stress analysis are plotted in polar graph form to show the areas of strain in micro inches at the outer surface of the skin and the inner lip of the stringer.
Constant thickness elastic conical shells subject to lateral loads, deriving asymptotic solution
1. Criteria are presented for the elastic instability of thin single and multilayer conical and cylindrical shells under combined axial load and external pressure. These criteria, used in design analysis, are based on theoretical results and the correlation of these results with readily available experimental data. 2. A summary is included of the studies at Avco RAD of shells under static or dynamic loads.
Effect of concentrated forces on thin walled elastic spherical shell
Discontinuity stress fields in thin elastic multicellular shell structures subject to inertial, pressure, and thermal loading
Elastic instability of pressurized cylindrical shells under compression or bending
A synopsis of a series of investigations into the instability of axially compressed cylindrical shells is given. The objective of the research, which was made with models, was to devise a technique of nondestructive evaluation. The results show that, with models at any rate, success was achieved. Probing methods which can be used to determine the locations of weakness and the pertinent instability load levels were devised. The research on large scale shells was undertaken to determine the critical loads under as uniform a circumferential distribution of axial compressive force as possible. It is clear from the results presented that this objective was met.
The problem of the finite displacement and buckling, of a shallow spherical dome is investigated both theoretically and experimentally. Experimental results seem to indicate that the classical criterion of buckling is applicable to very shallow spherical domes for which the theoretical calculation was made. A transition to energy criterion for higher domes is also indicated.
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Elastic-plastic deformation theories and elastic solutions method for solving problem of stress concentration around circular hole in spherical shell
Computer program for finite difference solutions of linear asymmetric bending of elastic thin shell of revolution under arbitrary loading
The buckling of a truncated elastic conical shell subjected to an axial compression is a classical problem in shell structures. The paper reinvestigates the buckling of an axially compressed truncated conical shell with rigid bulkheads. Two improvements are achieved. First, the condition that the total horizontal displacement must vanish due to rigid bulkhead and axisymmetry is treated as a constraint. This constraint is incorporated into the system through the use of the Lagrange multiplier; then the variational method is used to derive a complete set of boundary conditions for conical shells. Second, the stability is evaluated in the deformed state using the asymptotic solutions of the pair of Donnell-type equations for axisymmetric configuration. The results indicate that the buckling strength of conical shells depends mainly on the condition of the smaller end. In addition to the vertex angle, the distance ratio plays, at least, an equally important role.
Nonlinear finite deflection theory employed in analysis of general instability of elastic cylindrical shells - solutions obtained by minimum potential energy and Galerkin methods