Aluminum alloy 7449 in the T7651 temper is solution heat treated, stress relieved, and overaged. This processing produces an alloy of high strength, good corrosion/exfoliation resistance, and good toughness. An application of interest is the upper-wing skin of aircraft structures. This datasheet provides information on composition and tensile properties as well as fracture toughness. It also includes information on forming. Filing Code: AL-402. Producer or source: Pechiney Rolled Products LLC.

7499-T7651, aircraft structures, chemical composition, corrosion-resistant alloys, fracture toughness, tensile properties, workability
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2006
ASM International
Topics
Corrosion-resistant alloys Aluminum alloys Chemical composition Workability Fracture toughness Tensile properties Wings and wing structures
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