Mechanical-Property Data 7175 Aluminum: T736 Forging

Abstract

Aluminum alloy 7175 is a new Premium Strength Die Forging. This development is intended to provide relatively high strength/weight ratios for aerospace applications. The guaranteed minimum longitudinal yield strength for the -T736 temper is approximately 17 percent above the current minimum requirements of specifications covering 7075 alloy die forgings in the -T73 temper. Although the development emphasis was placed on high longitudinal strength, the transverse ductility is also well above that of most conventional 7075 die forgings. Tests on a limited number of forgings in the -T736 temper indicate that the stress-corrosion cracking threshold in the short transverse direction should be at least 35 ksi. Currently, the product is limited to closed die airframe-type forgings.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1970
Accession Number
AD0715878

Entities

Organizations

  • Battelle Memorial Institute

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Aluminum Alloys
  • Axial Loads
  • Contracts
  • Engineering
  • Government Procurement
  • Governments
  • Materials
  • Materials Engineering
  • Materials Laboratories
  • Mechanical Properties
  • Plastic Deformation
  • Stress Concentration
  • Stress Corrosion
  • Stresses
  • Yield Strength

Fields of Study

  • Materials science

Readers

  • Metallurgy

Technology Areas

  • Space