Large Deflections of Plates with Nonlinear Elasticity and Hollow Shells with Hinge-Supported Edges
Abstract
The method of finite differences was used to solve problems dealing with large deflections of rectangular plates with nonlinear elasticity and hollow shells with hinge-supported edges, which are under the effect of external normal pressure uniformly distributed along the entire surface or along the central rectangular area. The curvature parameter values at which a crack in a cylindrical panel occurs are established. Critical loads and their corresponding deflections were found for panels with different curvature parameters.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 26, 1973
- Accession Number
- AD0756103
Entities
People
- M. S. Kornishin
- N. I. Dedov
- N. N. Stolyarov
Organizations
- National Air and Space Intelligence Center