DETERMINATION OF PRINCIPAL PROPERTIES OF 'E' FIBER-GLASS HIGH TEMPERATURE EPOXY LAMINATES FOR AIRCRAFT

Abstract

A test program was conducted to develop mechanical strength data on ECDE 7581 glass fabric impregnated with F161 resin. This data is to be used in the new revision of MIL-HDBK-17. The properties determined were tensile, compressive and shear strengths and stiffnesses and Poisson's ratios over the temperature range of -65F to 450F. The results are presented in graphical, tabular, and summary forms.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1969
Accession Number
AD0699362

Entities

People

  • A. Slobodzinski
  • G. Lubin
  • J. A. Munyak
  • M. Rosenberg
  • S. J. Dastin

Organizations

  • Grumman

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Epoxy Laminates
  • Failure Mode And Effect Analysis
  • Flexural Properties
  • Laminates
  • Materials
  • Materials Processing
  • Mechanical Properties
  • Mechanical Working
  • Modulus Of Elasticity
  • Physical Properties
  • Quality Control
  • Shear Strength
  • Specific Gravity
  • Stress Strain Relations
  • Stresses
  • Tensile Strength
  • Test Methods

Readers

  • Climatology
  • Reinforced Composite Materials
  • Software Engineering