Statics of Thin-Walled Shells of Revolution
Abstract
The book is devoted to the theory and design of thin-walled shells of revolution. The basic equations of the theory are derived in an elementary form for a shell of revolution subjected to arbitrary loading. The deformations of cylindrical, conical, spherical, and toroidal shells are analyzed in detail under axisymmetrical and bending loads. The book is intended for design engineers and scientific workers engaged in designing machines and structures for strength.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 18, 1971
- Accession Number
- AD0727859
Entities
People
- V. S. Chernina
Organizations
- Air Force Systems Command