1. von Kármán, Th., andTsien, H. S., “The Buckling of Thin Cylindrical Shells Under Axial Compression,”J. Aeronaut. Sci., 8, 303–312 (1941).
2. Donnell, L. H., andWan, C. C., “Effects of Imperfections on Buckling of Thin Cylinders and Columns Under Axial Compression,”J. Appl. Mech., 17, 73–83 (1950).
3. Lockheed Missiles and Space Co., “The Effect of Axisymmetric Imperfections on the Buckling of Cylindrical Shells under Axial Compression,” by W. T. Koiter (Consultant), Report 6-90-63-86, Palo Alto, Calif., August 1963.
4. Babcock, C. D., and Sechler, E. E., “The Effect of Initial Imperfections on the Buckling Stress of Cylindrical Shells,” NASA TN D-1510, 135–141. December 1962.
5. Thielemann, W., “New Developments in the Nonlinear Theories of Buckling of Thin Cylindrical Shells,”Proc. Durand Centennial Conf., ed. by N. J. Hoff andW. G. Vincenti, Pergamon Press, New York, 1960.