Abstract
The problem considered in this paper is the determination of the stresses near a discontinuity of thickness and meridian curvature across a circle of latitude of a thin shell of revolution under internal pressure. It is assumed that there is no discontinuity of meridian slope, but an eccentricity between the middle surfaces on the two sides of the discontinuity is included. The derivation is based upon a non-linear theory for the boundary layer stresses which is valid when the normal deflexion of the shell is of the order of the thickness. Explicit expressions for the stresses are derived, with an accuracy of order √( t r ) .
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