Elevated-Temperature Compressive Stress-Strain Data for 24S-T3 Aluminum-Alloy Sheet and Comparisons with Extruded 75S-T6 Aluminum Alloy

Abstract

Results are presented of compressive stress-strain tests of 24S-T3 aluminum-alloys sheet at stabilized elevated temperatures up to 700 degrees F, exposure times of 1/2 to 2 hours, and strain rates of 0.002 to 0.006 per minute. Some general comparisons with extruded 75S-T6 aluminum alloy are included.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1949
Accession Number
ADA380675

Entities

People

  • George J. Heimerl
  • William M. Roberts

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Air Force
  • Air Force Facilities
  • Alloys
  • Aluminum
  • Aluminum Alloys
  • Dispersion Hardening
  • Materials
  • Modulus Of Elasticity
  • Strain Rate
  • Stress Strain Relations
  • Stresses

Readers

  • Mechanical Engineering/Mechanics of Materials.
  • Metallurgy