Bending of a Three-Layer Cylindrical Shell Reinforced with a Regular System of Rectangular Stiffeners,
Abstract
This article investigates the bending of a three-layer shallow shell under the effect of a transverse load. The shell is of symmetric construction in terms of thickness with isotropic bearing layers of thickness t and a light isotropic transversal filler of thickness 2h. The broken line hypothesis is used for the tangential displacements of the shell. Flexural rigidity of the external layers is not considered.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 24, 1974
- Accession Number
- AD0782535
Entities
People
- L. F. Vodyanoi
Organizations
- National Air and Space Intelligence Center