Analysis of an Axisymmetric, Orthotropic Shell of Revolution with Transverse Shear Deformations.
Abstract
A straight-line element is used to analyze an axisymmetric, orthotropic shell of revolution by the finite element method. Shear deformations are included. The element stiffness re-lations were obtained from the well-known principle of minimum potential energy. A computer program to implement the solution and the instructions for its usage are also reported. Example problems illustrating accuracy and usage are included. (Author-PL)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 20, 1974
- Accession Number
- AD0781976
Entities
People
- Charles M. Eldridge
- Ju-chin Huang
Organizations
- United States Army Aviation and Missile Command