Available Properties |
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- Density, AA; Typical
- Hardness, Brinell, AA; Typical; 500 g load; 10 mm ball
- Hardness, Knoop, Converted from Brinell Hardness Value
- Hardness, Rockwell A, Converted from Brinell Hardness Value
- Hardness, Rockwell B, Converted from Brinell Hardness Value
- Hardness, Vickers, Converted from Brinell Hardness Value
- Tensile Strength, Ultimate, AA; Typical
- Tensile Strength, Ultimate
- Tensile Strength, Ultimate
- Tensile Strength, Ultimate
- Tensile Strength, Ultimate
- Tensile Strength, Ultimate
- Tensile Strength, Ultimate
- Tensile Strength, Ultimate
- Tensile Strength, Ultimate
- Tensile Strength, Ultimate
- Tensile Strength, Ultimate
- Tensile Strength, Ultimate, Plate; T62, T651
- Tensile Strength, Ultimate, Plate; T62, T651
- Tensile Strength, Ultimate, Plate; T62, T651
- Tensile Strength, Ultimate, Sheet
- Tensile Strength, Ultimate, Sheet
- Tensile Strength, Ultimate, Plate; T62, T651
- Tensile Strength, Ultimate, Plate; T62, T651
- Tensile Strength, Ultimate, Sheet
- Tensile Strength, Ultimate, Sheet
- Tensile Strength, Ultimate, Plate; T62, T651
- Tensile Strength, Ultimate, Plate; T62, T651
- Tensile Strength, Yield, AA; Typical
- Tensile Strength, Yield, Plate; T62, T651
- Tensile Strength, Yield, Plate; T62, T651
- Tensile Strength, Yield, Plate; T62, T651
- Tensile Strength, Yield, Sheet
- Tensile Strength, Yield, Plate; T62, T651
- Tensile Strength, Yield, Sheet
- Tensile Strength, Yield, Plate; T62, T651
- Tensile Strength, Yield, Plate; T62, T651
- Tensile Strength, Yield, Sheet
- Tensile Strength, Yield, Plate; T62, T651
- Tensile Strength, Yield, Sheet
- Tensile Strength, Yield
- Tensile Strength, Yield
- Tensile Strength, Yield
- Tensile Strength, Yield
- Tensile Strength, Yield
- Tensile Strength, Yield
- Tensile Strength, Yield
- Tensile Strength, Yield
- Tensile Strength, Yield
- Tensile Strength, Yield
- Elongation at Break
- Elongation at Break
- Elongation at Break
- Elongation at Break
- Elongation at Break
- Elongation at Break
- Elongation at Break
- Elongation at Break
- Elongation at Break
- Elongation at Break
- Elongation at Break, Plate; T62, T651
- Elongation at Break, Sheet
- Elongation at Break, Plate; T62, T651
- Elongation at Break, Plate; T62, T651
- Elongation at Break, Plate; T62, T651
- Elongation at Break, Plate; T62, T651
- Elongation at Break, Sheet
- Elongation at Break, Plate; T62, T651
- Elongation at Break, Sheet
- Elongation at Break, Sheet
- Elongation at Break, Plate; T62, T651
- Elongation at Break, AA; Typical
- Elongation at Break, AA; Typical
- Modulus of Elasticity, AA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.
- Poissons Ratio
- Fatigue Strength, completely reversed stress; RR Moore machine/specimen
- Fracture Toughness, T651; Plate; S-L; average
- Fracture Toughness, T651; Plate; S-L
- Fracture Toughness, T651; Forgings; S-L
- Fracture Toughness, K(IC) in S-L Direction
- Fracture Toughness, T651; Plate; T-L
- Fracture Toughness, T651; Plate; T-L; average
- Fracture Toughness, K(IC) in T-L Direction
- Fracture Toughness, T651; Plate; L-T; average
- Fracture Toughness, T651; Plate; L-T
- Fracture Toughness, K(IC) in L-T Direction
- Machinability, 0-100 Scale of Aluminum Alloys
- Shear Modulus
- Shear Strength, AA; Typical
- Electrical Resistivity, AA; Typical
- CTE, linear
- CTE, linear
- CTE, linear, AA; Typical; average over range
- CTE, linear
- CTE, linear
- Specific Heat Capacity
- Thermal Conductivity, AA; Typical at 77°F
- Melting Point, AA; Typical range based on typical composition for wrought products >= 1/4 in. thickness. Homogenization may raise eutectic melting temperature 20-40°F but usually does not eliminate it.
- Solidus, AA; Typical
- Liquidus, AA; Typical
- Annealing Temperature
- Solution Temperature
- Aging Temperature
- Aluminum, Al, As remainder
- Chromium, Cr
- Copper, Cu
- Iron, Fe
- Magnesium, Mg
- Manganese, Mn
- Other, each
- Other, total
- Silicon, Si
- Titanium, Ti
- Zinc, Zn
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