Minimum Weight Design of Stiffened Circular Cylindrical Shells Subject to Destabilizing Load.
Abstract
This report contains a technical procedure by which one may design a fuselage type stiffened thin curcular cylindrical shell to carry safely a specified destabilizing load (uniform axial compression, uniform pressure, and torsion) individually applied.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 01, 1975
- Accession Number
- ADA017657
Entities
People
- George J. Simitses
- Jagannath Giri
- Mohan Aswani
Organizations
- Georgia Tech