SAE AMS 4329A Aluminum Alloy, Plate (7085-T7651) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged
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SAE AMS 4329A Document Information:
Title
Aluminum Alloy, Plate (7085-T7651) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged
SAE International
Publication Date:
May 1, 2006
Scope:
Form
This specification covers an aluminum alloy in the form of plate.
Application
This product has been used in aerospace applications requiring a high level of mechanical properties and fracture toughness, moderate resistance to stress-corrosion cracking and resistance to exfoliation corrosion, but usage is not limited to such applications.
Keywords:
- 7085-T7651
- fracture toughness
- Aluminum alloy plate
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