Affiliation:
1. Pratt & Whitney Aircraft, Connecticut Aircraft Nuclear Engine Laboratory, Middletown, Conn.
Abstract
An analysis is developed for bending of a thin circular cylindrical shell under a varying radial line load distributed around the circumference at the center section. The problem is solved by reducing the eighth-order differential equation of thin-shell theory to two approximate fourth-order equations. Deflections, bending stresses, and membrane stresses are evaluated. Both simply supported and clamped ends are considered.
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Cited by
7 articles.
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