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

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Distribution Statement:

APPROVED FOR PUBLIC RELEASE