Buckling of Eccentrically Loaded Curved Panels
Publication: Journal of Structural Engineering
Volume 109, Issue 9
Abstract
Determination of the feasibility of utilizing prefabricated, curved steel panels in the construction of tall cylindrical shells. A unique method of load testing curved panels was developed which allowed for the inclusion of actual elastic boundary conditions. A theoretical development is presented that includes both the effects of initial imperfections and eccentricity. The specific purpose of the research was to determine the buckling capacity of cold‐rolled, steel, curved panels and to investigate the effect stiffeners had on the buckling capacity. The research involved seventeen full scale tests on curved panels of 16, 14 and 12 gage thicknesses.
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References
1.
Almroth, B. O., “Postbuckling Behavior of Axially Compressed Circular Cylinders,” AIAA Journal, Vol. 1, No. 3, Mar., 1963, p. 630.
2.
Babcock, D. C., and Sechler, E. E., “The Effect of Initial Imperfections on the Buckling Stress of Cylindrical Shells,” Collected Papers on Instability of Shell Structures, NASA TN D‐1510, Washington, D.C., 1935, p. 135.
3.
Donnell, L. H., “A New Theory for the Buckling of Thin Cylinders under Axial Compression and Bending,” Transactions of the American Society of Mechanical Engineers, Vol. 56, 1934, p. 795.
4.
Donnell, L. H., and Wan, C. C., “Effect of Imperfections on the Buckling of Thin Cylinders and Columns under Axial Compression,” Journal of Applied Mechanics, Vol. 17, No. 1, Mar., 1950, p. 73.
5.
Seide, P., and Weingarten, V. I., “On the Buckling of Circular Cylindrical Shells Under Pure Bending,” Journal of Applied Mechanics, Vol. 28, Mar., 1961, p. 112.
6.
Sokol, Ted T., “Determination of the Buckling Capacity of Eccentrically Loaded Steel Cylindrical Panels,” dissertation presented to Kansas State University, Manhattan, Kans., Mar., 1982, in partial fulfillment of the requirements for the degree of Doctor of Philosophy.
7.
Stein, M., “The Influence of Prebuckling Deformations and Stresses on the Buckling of Perfect Cylinders,” NASA TR R‐190, Washington, D.C., Feb., 1964.
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Copyright © 1983 ASCE.
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Published online: Sep 1, 1983
Published in print: Sep 1983
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