AA 5657

Alloy Digest ◽  
1991 ◽  
Vol 40 (6) ◽  

Abstract AA 5657 is a binary aluminum/magnesium alloy of moderate strength. It is not hardenable by heat treatment. It is strain hardenable. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-317. Producer or source: Various aluminum companies.

Alloy Digest ◽  
1978 ◽  
Vol 27 (11) ◽  

Abstract ALUMINUM 5005 is nominally an aluminum-magnesium alloy that cannot be hardened or strengthened by heat treatment; however, it can be hardened by cold working. It has excellent resistance to corrosion, excellent weldability and good brazeability. Its numerous applications include appliances, utensils and architectural components. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-38. Producer or source: Various aluminum companies. Originally published April 1956, revised April 1973, revised November 1978.


Alloy Digest ◽  
1992 ◽  
Vol 41 (3) ◽  

Abstract AA 5052 is a non heat treatable aluminum/magnesium alloy of moderate strength and good weldability. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-322. Producer or source: Various aluminum companies.


Alloy Digest ◽  
1960 ◽  
Vol 9 (1) ◽  

Abstract MAGNESIUM ALLOY-TA54A is a general purpose hammer-forging alloy having intermediate strength. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Mg-44. Producer or source: Aluminum Company of America.


Alloy Digest ◽  
1984 ◽  
Vol 33 (10) ◽  

Abstract ALUMINUM 328.0 is an aluminum-silicon-copper-magnesium alloy that responds to heat treatment. It retains good strength up to 400 F. The machinability of this alloy is fair. Its uses include cylinder blocks, crankcases, gear housings and similar components. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on high temperature performance and corrosion resistance as well as casting, heat treating, and machining. Filing Code: Al-253. Producer or source: Various aluminum companies.


Alloy Digest ◽  
1983 ◽  
Vol 32 (9) ◽  

Abstract ALUMINUM 710.0 is a natural-aging aluminum alloy produced by sand casting. It develops high mechanical properties without a quenching heat treatment. This alloy has high resistance to shock and excellent resistance to corrosion. Aluminum 710.0 is recommended for highly stressed castings. This datasheet provides information on composition, physical properties, hardness, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-247. Producer or source: Various aluminum companies.


Alloy Digest ◽  
2021 ◽  
Vol 70 (11) ◽  

Abstract Atlas 5005 is a non-heat-treatable, aluminum-magnesium alloy. This alloy has been widely adopted for anodized architectural panels. With correct rolling practices and composition controls, Atlas 5005 architectural sheet provides exceptionally high-quality surfaces after anodizing. The architectural products produced from this alloy are used on many high-end building projects to meet customer specifications for uniformity and color match. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-482. Producer or source: Atlas Steels.


Alloy Digest ◽  
1981 ◽  
Vol 30 (5) ◽  

Abstract ALUMINUM 6463 is an aluminum-magnesium-silicon alloy used widely for extrusions. It can be hardened and strengthened by a precipitation-hardening heat treatment. Its many applications comprise extrusions for trim and archtectural use in the automotive, appliance and building industries. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-189. Producer or source: Various aluminum companies. Originally published August 1969, revised May 1981.


Alloy Digest ◽  
1991 ◽  
Vol 40 (9) ◽  

Abstract AA 6351 wrought alloy contains silicon and magnesium in such amounts that Mg2Si is present as the precipitation hardening constituent with proper heat treatment. The 6000 series alloys are less strong than most of the 2000 and 7000 series aluminum alloys. The formability and corrosion resistance of AA 6351 are good. This datasheet provides information on composition, physical properties, hardness, tensile properties, and shear strength as well as fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-319. Producer or source: Various aluminum companies.


Alloy Digest ◽  
1958 ◽  
Vol 7 (9) ◽  

Abstract Aluminum 5456 is an aluminum-magnesium alloy suitable for structural welding applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on forming, heat treating, machining, and joining. Filing Code: Al-70. Producer or source: Aluminum Company of America.


Alloy Digest ◽  
1994 ◽  
Vol 43 (1) ◽  

Abstract INCONEL ALLOY 725 is an age-hardenable alloy that displays high strength along with excellent ductility and toughness. Its corrosion resistance is comparable to alloy 625. Good flattening properties are exhibited in age-hardened tubing. This datasheet provides information on composition, physical properties, hardness, tensile properties, and shear strength as well as fracture toughness. It also includes information on corrosion resistance as well as heat treating and machining. Filing Code: Ni-445. Producer or source: Inco Alloys International Inc.


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