Strength Analysis and Design of Multilayered Thick Composite Spherical Pressure Vessels

Abstract

A design study of a multilayered spherical composite pressure vessel is presented. Each layer of the vessel is composed of quasi-isotropic layups of composite plies. For the stress analysis, however, each layer is assumed to be homogeneous whose three dimensional properties are equivalent to that of the quasi-isotropic plies. The linear theory of elasticity is employed so that the analysis is not limited to any thickness of the vessel. For the strength analysis the Tsai-Wu failure criterion is used. Using the ply constitutive law and lamination angle, the ply stresses and strains are determined from the layer stress strain relations. Then the failure criterion is used for each ply. The objective of this study is to design a spherical vessel with an acceptable safety factor to operate at an internal pressure of 200 MPa. In view of the winding and manufacturing difficulties, a design restriction of b/a < or = 1.25 was set for this design. However a two-layered hybrid sphere of b/a = 1.25 (b: outer radius, a: inner radius) with T300/5208 and IM6/epoxy outside is considered to be an acceptable design.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1991
Accession Number
ADA236266

Entities

People

  • Ajit K. Roy

Organizations

  • University of Dayton

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Composite Materials
  • Compressive Strength
  • Elastic Properties
  • Epoxy Composites
  • Failure Mode And Effect Analysis
  • Graphite Epoxy Composites
  • Internal Pressure
  • Laminates
  • Materials
  • Materials Laboratories
  • Pressure Vessels
  • Stress Analysis
  • Stress Strain Relations
  • Stresses
  • Thickness
  • Three Dimensional
  • Universities

Readers

  • Fluid Dynamics.
  • Reinforced Composite Materials
  • Structural Health Monitoring of Composite Structures.