Minimum Weight Design of Fuselage Type Stiffened Circular Cylindrical Shells Subject to Uniform Axial Compression,
Abstract
This report contains a technical procedure by which one may design a fuselage-type stiffened thin circular cylindrical shell to carry safely a specified uniform axial compression with minimum weight.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 1974
- Accession Number
- ADA004412
Entities
People
- George J. Simitses
- Variddhi Ungbhakorn
Organizations
- Georgia Tech