EFFECT OF HEATING ALUMINUM ALLOY WING STRUCTURE TO 325 F ON THE MECHANICAL PROPERTIES OF ITS COMPONENT MATERIALS

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Document Details

Document Type
Technical Report
Publication Date
Jul 07, 1959
Accession Number
AD0402171

Entities

People

  • H. C. Turner
  • P.w. Bergstedt
  • W. M. Sutherland

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Alloys
  • Aluminum
  • Aluminum Alloys
  • Elongation
  • Extrusion
  • Materials
  • Materials Testing
  • Mechanical Properties
  • Tensile Properties
  • Tensile Strength
  • Test Methods
  • Yield Strength