Creep Buckling of Plates and Shells

Creep Buckling of Plates and Shells
Author: Stanford University. Department of Aeronautics and Astronautics
Publisher:
Total Pages: 66
Release: 1972
Genre:
ISBN:

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A review is presented of the fundamental considerations that enter into the calculation of the buckling of plates and shells whose material deforms in consequence of nonlinear creep. Results are given of analyses that have been carried out for flat plates subjected to edge-wise compression and for circular cylindrical shells subjected to uniform axial compression, to a uniform external pressure and to a constant bending moment. The character of the behavior of these structural elements after buckling is also discussed. (Author).

On the Creep Buckling of Axially Compressed Circular Cylindrical Shells

On the Creep Buckling of Axially Compressed Circular Cylindrical Shells
Author: Bernard Robert Schneider
Publisher:
Total Pages: 104
Release: 1966
Genre: Buckling (Mechanics)
ISBN:

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The problem of creep induced instability in structures is discussed. A linearization procedure proposed by Onat and Wang (Creep in Structures, Springer-Verlag, 1962, p. 125) and generalized by Carlson (Recent Progress in Applied Mechanics - The Folke Odgvist Volume, Almqvist and Wiksell, Gebers, Stockholm, 1966) is applied to the problem of the creep buckling of circular cylindrical shells under uniform, axial compression. Solutions for axisymmetric creep buckling of semi-infinite and infinite cylinders are obtained and a comparison with experimental data is made. In accordance with expectations based on the criterion for instability, the theoretically predicted critical times are smaller than the experimentally observed critical times.

Experimental Study of the Creep Buckling of Moderately Thin-walled Circular Cylindrical Shells Subjected to Axial Compression

Experimental Study of the Creep Buckling of Moderately Thin-walled Circular Cylindrical Shells Subjected to Axial Compression
Author: Michel Benoit
Publisher:
Total Pages: 144
Release: 1970
Genre: Buckling (Mechanics)
ISBN:

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Test equipment suitable for the study of the creep buckling of axially compressed circular cylindrical shells was developed and built. With the aid of this equipment, thirty-one electroformed nickel cylinders of radius-to-thickness ratios ranging from 30.6 to 96.4 were tested at a temperature of 650F. The loading of each specimen was interrupted usually once, and in some cases twice, to permit an exact measurement of the creep deformations produced by the axial compression. Diagrams showing the deformed shapes of eight generators of each specimen are presented at two or three stages of the creep buckling process. Inspection of the figures reveals that specimens of this kind either buckle axisymmetrically, or begin the creep buckling process in a axisymmetric manner but change over to a multilobed pattern in later stages of the deformations. (Author).

The Effect of Variations in the Creep Exponent N on the Buckling of Circular Cylindrical Shells in Axial Compression

The Effect of Variations in the Creep Exponent N on the Buckling of Circular Cylindrical Shells in Axial Compression
Author: Terence Chase Honikman
Publisher:
Total Pages: 192
Release: 1970
Genre: Buckling (Mechanics)
ISBN:

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The purpose of the investigation is to determine the effect of creep on the load carrying capability of axially symmetric circular cylinders when subjected to uniform axial compression. In particular, the effect of variation of the creep exponent in Odgvist's bi-axial creep law for creep, is investigated. The analysis of the problem is undertaken in the cases in which the creep exponent has the value one and five. Closed form analytical results are presented for the cases in which the creep exponent has the value one, three, and five. Two numerical procedures are developed. The first generates the governing equations of the creep problem symbolically, while the second solves these equations. Numerical results are presented for the cases in which the creep exponent has the value three, five, seven, and nine. The numerical results are compared with the analytical results. While the numerical programs offer a means of further extending the range of values of the creep exponent, this is carried out instead by two empirical methods, which are based on the numerical results already obtained. The case in which the creep exponent becomes unbounded is considered analytically. Dimensionless plots of radial displacement versus time are presented for each value of the creep exponent, and for a variety of values of initial imperfections in the shell wall. A simple graphical method is developed by which the plot for any given value of the initial imperfection may be obtained from another similar plot for which the value of the initial imperfection is smaller than the given value. (Author).

Creep Buckling of Circular Cylindrical Shells in Pure Bending

Creep Buckling of Circular Cylindrical Shells in Pure Bending
Author: Stanford University. Department of Aeronautics and Astronautics
Publisher:
Total Pages: 62
Release: 1970
Genre: Buckling (Mechanics)
ISBN:

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The two simultaneous nonlinear first-order differential equations characterizing the problems that were derived by the senior author in a paper in 1956 and were at that time solved for a few cases by numerical integration are solved here analytically with the aid of a few simplifying assumptions. The very simple formula derived in this manner is used to compute the critical times of a series of shells tested in the laboratory. It is found that the formula predicts somewhat larger values for the critical time than the experimental results. (Author).

Buckling of Shell Structures, on Land, in the Sea and in the Air

Buckling of Shell Structures, on Land, in the Sea and in the Air
Author: J.F. Jullien
Publisher: CRC Press
Total Pages: 539
Release: 1991-09-09
Genre: Architecture
ISBN: 1482286734

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This book provides better inputs for improvement of the buckling load predictions of stiffened cylindrical shells subjected to combined loading. It is based on the International Colloquium Buckling of shell structures, on land, in the sea and in the air, Lyon, France, 17 September 1991.

Creep Buckling of Relatively Thick Circular Cylindrical Shells Compressed Axially

Creep Buckling of Relatively Thick Circular Cylindrical Shells Compressed Axially
Author: Stanford University. Department of Aeronautics and Astronautics
Publisher:
Total Pages: 34
Release: 1973
Genre: Buckling (Mechanics)
ISBN:

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Experimental results obtained with 31 nickel circular cylindrical shell specimens are evaluated in the light of the theory. The test results have already been reported in SUDAAR No. 415. The experimental creep buckling times obtained in axial compression at a temperature of 650F were found to be in reasonable agreement with the theoretical formulas. (Author).