CIRCULAR CYLINDRICAL SHELLS UNDER SEGMENTAL CIRCUMFERENTIAL LINE LOAD,
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1963
- Accession Number
- AD0419923
Entities
People
- James Sheng
- Joseph Kempner
Organizations
- New York University Tandon School of Engineering