Residual Stress and High-Temperature Creep Behavior in Carbon-Carbon Composites,

Abstract

Residual stress is measured in a carbon-carbon composite. The curvature of a slice of asymmetric cross section indicates the amount of stress caused by thermal expansion anisotropy. Measured high-temperature creep rates are used to estimate stress relaxation times at high temperatures. (MM)

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Document Details

Document Type
Technical Report
Publication Date
Sep 30, 1987
Accession Number
ADA302261

Entities

People

  • L. A. Feldman

Organizations

  • The Aerospace Corporation

Tags

Communities of Interest

  • Advanced Electronics
  • Sensors
  • Space

DTIC Thesaurus Topics

  • Carbon Carbon Composites
  • Chemical Kinetics
  • Chemical Reactions
  • Chemistry
  • Composite Materials
  • Curvature
  • High Temperature
  • Materials
  • Materials Science
  • Mechanical Properties
  • Mechanics
  • Physics Laboratories
  • Relaxation Time
  • Residual Stress
  • Semiconductor Devices
  • Space Systems
  • Thermal Expansion

Readers

  • Mechanical Engineering/Mechanics of Materials.
  • Surface Engineering/Surface Coating Technology.