The Analysis of Inflatable Antennas Using A Corotational Finite Element Approach

Abstract

The Jaumann stress strain approach has been used to evaluate a nonlinear structural response to a shell like geometry. The method employs a finite element solution incorporating the Jaumarin stress-strain relationships b d on large displacement and large rotation using a corotational technique. It is possible to evaluate the effects of irect and shear stresses within a laminated structure. Results show that the need for a correct thorough evaluation of the stresses of the shell is required as the shell thickness increases relative to the resulting geometry. In a predominately membrane resistant structure, the three types of theories, Eulerian, Jaumann and Lagrangian show close" comparison.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1998
Accession Number
ADA353813

Entities

People

  • Anthony N. Palazotto
  • J. O. Chol

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Cartesian Coordinates
  • Composite Materials
  • Coordinate Systems
  • Epoxy Composites
  • Equations
  • Geometry
  • Graphite Epoxy Composites
  • Internal Pressure
  • Materials
  • Membranes
  • Radial Stress
  • Shape
  • Shear Stresses
  • Space Systems
  • Stresses
  • Thickness

Readers

  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Structural Dynamics.