Abstract
It can be seen easily that the expressions for stresses and displacements using Eqs. (3) and (10) will be the same as given by Eq. (21) in Ref. 1. Numerical integration to evaluate these stresses and displacements can be done as explained in Ref. 1. References 1 Klosner, J. M., The elasticity solution of a long circularcylindrical shell subjected to a uniform, circumferential, radial line load, J. Aerospace Sci. 29, 834-841 (1962). 2 Tranter, C. J. and Craggs, J. W., The stress distribution in a long circular cylinder when a discontinuous pressure is applied to the curved surface, Phil. Mag. 36, 241-250 (1945). 3 Fliigge, W. (ed.), Handbook of Engineering Mechanics (McGraw-Hill Book Co., Inc., New York, 1962), pp. 41-15-41-16.
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