POST-CRITICAL DEFORMATIONS OF A SHORT CYLINDRICAL SHELL AND A SQUARE PANEL UNDER AXIAL COMPRESSION,
Abstract
The buckling and postbuckling deformation of a cylindrical panel between stringers and lateral frames of a circular cylindrical shell under axial compression as well as of the shell itself is investigated by using the A. V. Pogorelov method.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 14, 1969
- Accession Number
- AD0693477
Entities
People
- V. V. Nykhailov
Organizations
- National Air and Space Intelligence Center