The buckling of a free edge of an axially-compressed circular cylindrical shell
Authors:
W. Nachbar and N. J. Hoff
Journal:
Quart. Appl. Math. 20 (1962), 267-277
MSC:
Primary 73.35
DOI:
https://doi.org/10.1090/qam/140215
MathSciNet review:
140215
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Additional Information
- Y. C. Fung and E. E. Sechler, Instability of thin elastic shells, Structural mechanics, Pergamon Press, New York, 1960, pp. 115–168. MR 0136149
N. J. Hoff, Buckling of thin shells, Von Kármán 80th Anniversary Lecture, May 11, 1961, to be published by the Institute of the Aerospace Sciences; see also SUDAER No. 114, Department of Aeronautical Engineering, Stanford University, 1961
L. H. Donnell, A new theory for the buckling of thin cylinders under axial compression and bending, Trans. A. S. M. E., 56, (1934) 795–806
W. Nachbar, Discontinuity stresses in pressurized thin shells of revolution Report LMSD-48483, Lockheed Missiles and Space Division, Sunnyvale, California, 1959
S. Timoshenko and S. Woinowsky-Krieger, Theory of plates and shells, second edition, McGraw-Hill, New York, 1959, pp. 432, 508, 512, 518, 523
- A. E. H. Love, A treatise on the Mathematical Theory of Elasticity, Dover Publications, New York, 1944. Fourth Ed. MR 0010851
W. Nachbar, Characteristic roots for Donnell’s equations with uniform axial prestress, SUDAER No. 108, Department of Aeronautical Engineering, Stanford University, July 1961, to be published in the Journal of Applied Mechanics
W. Nachbar and N. J. Hoff, On edge buckling of axially-compressed, circular cylindrical shells, SUDAER No. 115, Department of Aeronautical Engineering, Stanford University, November 1961
Y. C. Fung and E. E. Sechler, Instability of thin elastic shells, Structural Mechanics, Proceedings of the First Symposium on Naval Structural Mechanics, ed. by J. N. Goodier and N. J. Hoff, Pergamon Press, N. Y., 1960, pp. 115–168
N. J. Hoff, Buckling of thin shells, Von Kármán 80th Anniversary Lecture, May 11, 1961, to be published by the Institute of the Aerospace Sciences; see also SUDAER No. 114, Department of Aeronautical Engineering, Stanford University, 1961
L. H. Donnell, A new theory for the buckling of thin cylinders under axial compression and bending, Trans. A. S. M. E., 56, (1934) 795–806
W. Nachbar, Discontinuity stresses in pressurized thin shells of revolution Report LMSD-48483, Lockheed Missiles and Space Division, Sunnyvale, California, 1959
S. Timoshenko and S. Woinowsky-Krieger, Theory of plates and shells, second edition, McGraw-Hill, New York, 1959, pp. 432, 508, 512, 518, 523
A. E. H. Love, A treatise on the mathematical theory of elasticity, fourth edition, Dover, New York, 1944, pp. 517–522
W. Nachbar, Characteristic roots for Donnell’s equations with uniform axial prestress, SUDAER No. 108, Department of Aeronautical Engineering, Stanford University, July 1961, to be published in the Journal of Applied Mechanics
W. Nachbar and N. J. Hoff, On edge buckling of axially-compressed, circular cylindrical shells, SUDAER No. 115, Department of Aeronautical Engineering, Stanford University, November 1961
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Article copyright:
© Copyright 1962
American Mathematical Society
