The Relation between the Tensile Properties and Constitution of Aluminium-Rich Aluminium-Magnesium-Manganese-Zinc Alloys

Abstract

In view of the high tensile properties obtained on aluminium alloys of nominal composition 3% of magnesium, 1% of manganese and 7% of zinc in the wrought and heat treated condition, it was considered desirable to ascertain the effects of wide variations in the magnesium and zinc contents on the tensile properties and microstructure.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1946
Accession Number
ADA800722

Entities

People

  • A. H. Ross

Organizations

  • Royal Aircraft Establishment

Tags

Communities of Interest

  • Advanced Electronics

DTIC Thesaurus Topics

  • Aircrafts
  • Aluminum
  • Aluminum Alloys
  • Chromium
  • Elongation
  • Grain Boundaries
  • Hardness
  • Heat Treatment
  • Manganese
  • Materials
  • Metals
  • Physical Properties
  • Precipitation
  • Solution Heat Treatment
  • Stress Corrosion
  • Tensile Properties
  • Tensile Strength

Fields of Study

  • Materials science

Readers

  • Powder metallurgy of Titanium alloys.