Stress Corrosion Resistance of 7010-T73651

Abstract

7010-T73651 Aluminum Alloy was compared to 7050-T73651 in stress corrosion and exfoliation tests. Results of a 30 day alternate immersion test in 3 1/2 percent NaCl indicate that 7010-T73651 has a threshold stress of 35 ksi (240 MPa) and is resistant to exfoliation. The threshold stress for cracking of the 7050-T73651 was 45 ksi (310 MPa). (Author)

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Document Details

Document Type
Technical Report
Publication Date
Apr 16, 1980
Accession Number
ADA086150

Entities

People

  • L. A. Biggs

Organizations

  • Naval Air Warfare Center Warminster

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Alloys
  • Aluminum
  • Aluminum Alloys
  • Corrosion
  • Corrosion Resistance
  • Diameters
  • Exfoliation
  • Materials
  • Mechanical Properties
  • Resistance
  • Stress Corrosion
  • Stress Corrosion Cracking
  • Stresses
  • Tensile Properties
  • Tensile Strength
  • Tensile Stress

Fields of Study

  • Materials science

Readers

  • Mathematics or Statistics
  • Structural Health Monitoring of Composite Structures.