Buckle Contours in an Axially Compressed Circular Cylindrical Shell
Abstract
Experimentally determined buckle contours at initial instability for an axially compressed aluminum right circular cylinder of 3.35 inches in diameter and 0.0025 inch of wall thickness are presented and analyzed. The results show that for buckle amplitudes of as low as 2.8 times the wall thickness there is strong evidence of plastic deformation.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1971
- Accession Number
- AD0733374
Entities
People
- W. H. Horton
- Wayne Johnson
Organizations
- Stanford University