Accession Number:
AD0419923
Title:
CIRCULAR CYLINDRICAL SHELLS UNDER SEGMENTAL CIRCUMFERENTIAL LINE LOAD,
Descriptive Note:
Corporate Author:
POLYTECHNIC INST OF BROOKLYN N Y
Personal Author(s):
Report Date:
1963-04-01
Pagination or Media Count:
53.0
Abstract:
Equations for the deflections of and the stresses in thin-walled circular cylindrical shells simply supported at their ends and under segmental circumferential line-loads are determined. These loads consist of a uniformly distributed segmental radial load yielding a resultant radial force at the midpoint of a generator, a piecewise, uniformly distributed radial load statically equivalent to a concentrated circumferential moment at the midpoint of a generator, and a uniformly distributed longitudinal moment statically equivalent to a concentrated axial moment applied at the midpoint of a generator. Practical applications of the solutions given are indicated for solutions of problems involving loadings other than those specifically treated. Author