Paper shows how to obtain ordinary differential equations which determine distributed stresses when concentrated load is applied to ring of reinforced thin-walled cylinder; general approach developed permits applied force to have arbitrary direction; account is taken of flexure perpendicular to plane and torsion and flexure in plane; strain energy is taken to consist of 5 separate terms which are given; pertinence to aircraft fuselages and rockets.
Theory of ring-stiffened cylinders
J Aerospace Sciences
Journal of Aerospace Science ; 28 , n 9
1961
8 pages
Article (Journal)
English
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