THE PROBLEM OF SELECTING THE OPTIMUM STRUCTURE FOR FIBER GLASS-REINFORCED PLASTIC IN THIN ELASTIC SHELLS OF REVOLUTION,

Abstract

The property of controllable anisotropy is taken as the fundamental variable in analyzing the possibilities for calculating the optimum structure for fiberglass-reinforced plastic in nonuniform shells of revolution operating under zero-moment stressed-state conditions with regard to the effect of the binder. The problem is solved from the condition of least pliability of the shell with respect to a specific type of deformation under the effect of the applied form of loading. The most effective reinforcing structure is defined as that in which the anisotropy provides maximum rigidity with respect to a given load. The solution is given in terms of the winding angle corresponding to minimum deformation. Formulas are derived for determining the optimum winding angle for cylindrical, barrel-shaped and tapered shells under various types of loads with various boundary conditions. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 03, 1968
Accession Number
AD0684669

Entities

People

  • A. V. Chigirinskii

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Anisotropy
  • Boundaries
  • Elastic Shells
  • Fiberglass
  • Nonuniform
  • Physical Properties
  • Revolutions
  • Rigidity
  • Shells (Structural Forms)
  • Structural Components

Readers

  • Microwave Engineering.
  • Reinforced Composite Materials
  • Structural Dynamics.