Viscoelastic Analysis of Composite Flywheels for Energy Storage

Abstract

A viscoelastic analysis has been developed to investigate stress relaxation and creep in a multilayered composite cylinder subjected to rotation. The analysis accounts for ply-by-ply variation of material properties, fiber orientations, and density gradients through the thickness of cylinders. A closed form solution based on the corresponding elastic problem is derived for a generalized plane strain state in a thick-walled, multilayered cylinder. Laplace transform is then applied to obtain the numerical solution of the viscoelastic problem. This report illustrates the derivation of the analytical model and solution procedure. A numerical simulation shows substantial creep and stress relaxation in thick-walled cylinders at an elevated temperature. Viscoelastic effects of composite can result in a drastic change of stress and strain profiles in a cylinder over a period of time, which is critical in terms of structural durability for applications such as energy storage flywheels.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 2001
Accession Number
ADA396880

Entities

People

  • Jerome T. Tzeng

Organizations

  • United States Army Research Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Composite Materials
  • Constitutive Equations
  • Energy
  • Energy Storage
  • Equations
  • Flywheels
  • Materials
  • Materials Science
  • Mechanics
  • Military Research
  • Orientation (Direction)
  • Radial Stress
  • Rotation
  • Simulations
  • Storage
  • Surface Warfare
  • Warfare

Readers

  • Calculus or Mathematical Analysis
  • Structural Dynamics.
  • Structural Health Monitoring of Composite Structures.