STABILITY OF SHELLS OF REVOLUTION: GENERAL THEORY AND APPLICATION TO THE TORUS
Abstract
Contents: The elastic law; Equations of equilibrium; Shells of revolution under axially symmetric loads; Toroidal shell under external pressure-theoretical analysis; Toroidal shell under external pressure-numerical results; Free vibrations of prestressed shells of revolution.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 01, 1965
- Accession Number
- AD0617197
Entities
People
- L. H. Sobel
- W. Flugge
Organizations
- Lockheed Martin Missiles and Space