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Alclad Aluminum 7075-T6, T651Subcategory: 7000 Series Aluminum Alloy; Aluminum Alloy; Metal; Nonferrous MetalClose Analogs: Composition Notes: Composition for AA 7075 (not Alclad 7075 specifically).Aluminum content reported is calculated as remainder.Composition information provided by the Aluminum Association and is not for design.Key Words: Alclad 7075-T6, T651; Alclad 7075-T6, T651ComponentWt. %Al87.1 - 91.4Cr0.18 - 0.28Cu1.2 - 2FeMax 0.5ComponentWt. %Mg2.1 - 2.9MnMax 0.3Other, eachMax 0.05Other, totalMax 0.15ComponentWt. %SiMax 0.4TiMax 0.2Zn5.1 - 6.1Material Notes: Data points with the AA note have been provided by the Aluminum Association, Inc. and are NOT FOR DESIGN.Click here to view available vendors for this material.Physical PropertiesMetricEnglishCommentsDensity2.81g/cc0.102lb/inFor AA7075 (Not Alclad)Mechanical PropertiesUltimate Tensile Strength524MPa76000psiAA; TypicalTensile Yield Strength462MPa67000psiAA; TypicalElongation at Break11%11%AA; Typical; 1/16 in. (1.6 mm) ThicknessModulus of Elasticity71.7GPa10400ksiAA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.Shear Strength317MPa46000psiAA; TypicalProcessing PropertiesAnnealing Temperature413C775FSolution Temperature466 - 482C870 - 900FAging Temperature121C250FAluminum 7075-T6; 7075-T651Subcategory: 7000 Series Aluminum Alloy; Aluminum Alloy; Metal; Nonferrous MetalClose Analogs: Composition Notes: A Zr + Ti limit of 0.25 percent maximum may be used with this alloy designation for extruded and forged products only, but only when the supplier or producer and the purchaser have mutually so agreed. Agreement may be indicated, for example, by reference to a standard, by letter, by order note, or other means which allow the Zr + Ti limit.Aluminum content reported is calculated as remainder.Composition information provided by the Aluminum Association and is not for design.Key Words: Aluminium 7075-T6; Aluminium 7075-T651, UNS A97075; ISO AlZn5.5MgCu; Aluminium 7075-T6; Aluminium 7075-T651; AA7075-T6ComponentWt. %Al87.1 - 91.4Cr0.18 - 0.28Cu1.2 - 2FeMax 0.5ComponentWt. %Mg2.1 - 2.9MnMax 0.3Other, eachMax 0.05Other, totalMax 0.15ComponentWt. %SiMax 0.4TiMax 0.2Zn5.1 - 6.1Material Notes: General 7075 characteristics and uses (from Alcoa): Very high strength material used for highly stressed structural parts. The T7351 temper offers improved stress-corrosion cracking resistance.Applications: Aircraft fittings, gears and shafts, fuse parts, meter shafts and gears, missile parts, regulating valve parts, worm gears, keys, aircraft, aerospace and defense applications; bike frames, all terrain vehicle (ATV) sprockets.Data points with the AA note have been provided by the Aluminum Association, Inc. and are NOT FOR DESIGN.Click here to view available vendors for this material.Physical PropertiesMetricEnglishCommentsDensity2.81g/cc0.102lb/inAA; TypicalMechanical PropertiesHardness, Brinell150150AA; Typical; 500 g load; 10 mm ballHardness, Knoop191191Converted from Brinell Hardness ValueHardness, Rockwell A53.553.5Converted from Brinell Hardness ValueHardness, Rockwell B8787Converted from Brinell Hardness ValueHardness, Vickers175175Converted from Brinell Hardness ValueUltimate Tensile Strength572MPa83000psiAA; TypicalTensile Yield Strength503MPa73000psiAA; TypicalElongation at Break11%11%AA; Typical; 1/16 in. (1.6 mm) ThicknessElongation at Break11%11%AA; Typical; 1/2 in. (12.7 mm) DiameterModulus of Elasticity71.7GPa10400ksiAA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.Poissons Ratio0.330.33Fatigue Strength159MPa23000psiAA; 500,000,000 cycles completely reversed stress; RR Moore machine/specimenFracture Toughness20MPa-m18.2ksi-inK(IC) in S-L DirectionFracture Toughness25MPa-m22.8ksi-inK(IC) in T-L DirectionFracture Toughness29MPa-m26.4ksi-inK(IC) in L-T DirectionMachinability70%70%0-100 Scale of Aluminum AlloysShear Modulus26.9GPa3900ksiShear Strength331MPa48000psiAA; TypicalElectrical PropertiesElectrical Resistivity5.15e-006ohm-cm5.15e-006ohm-cmAA; Typical at 68FThermal PropertiesCTE, linear 68F23.6m/m-C13.1in/in-FAA; Typical; Average over 68-212F range.CTE, linear 250C25.2m/m-C14in/in-FAverage over the range 20-300CSpecific Heat Capacity0.96J/g-C0.229BTU/lb-FThermal Conductivity130W/m-K900BTU-in/hr-ft-FAA; Typical at 77FMelting Point477 - 635C890 - 1175FAA; Typical range based on typical composition for wrought products 1/4 inch thickness or greater. Homogenization may raise eutectic melting temperature 20-40F but usually does not eliminate eutectic melting.Solidus477C890FAA; TypicalLiquidus635C1175FAA; TypicalProcessing PropertiesAnnealing Temperature413C775FSolution Temperature466 - 482C870 - 900FAging Temperature121C250FAlclad Aluminum 7075-OSubcategory: 7000 Series Aluminum Alloy; Aluminum Alloy; Metal; Nonferrous MetalClose Analogs: Composition Notes: Composition for AA 7075 (not Alclad 7075 specifically).Aluminum content reported is calculated as remainder.Composition information provided by the Aluminum Association and is not for design.Key Words: Alclad 7075-O; Alclad 7075-OComponentWt. %Al87.1 - 91.4Cr0.18 - 0.28Cu1.2 - 2FeMax 0.5ComponentWt. %Mg2.1 - 2.9MnMax 0.3Other, eachMax 0.05Other, totalMax 0.15ComponentWt. %SiMax 0.4TiMax 0.2Zn5.1 - 6.1Material Notes: Data points with the AA note have been provided by the Aluminum Association, Inc. and are NOT FOR DESIGN.Click here to view available vendors for this material.Physical PropertiesMetricEnglishCommentsDensity2.81g/cc0.102lb/inFor AA7075 (Not Alclad)Mechanical PropertiesUltimate Tensile Strength221MPa32000psiAA; TypicalTensile Yield Strength96.5MPa14000psiAA; TypicalElongation at Break17%17%AA; Typical; 1/16 in. (1.6 mm) ThicknessModulus of Elasticity71.7GPa10400ksiAA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.Shear Strength152MPa22000psiAA; TypicalProcessing PropertiesAnnealing Temperature413C775FSolution Temperature466 - 482C870 - 900FAluminum 7075-OSubcategory: 7000 Series Aluminum Alloy; Aluminum Alloy; Metal; Nonferrous MetalClose Analogs: Composition Notes: A Zr + Ti limit of 0.25 percent maximum may be used with this alloy designation for extruded and forged products only, but only when the supplier or producer and the purchaser have mutually so agreed. Agreement may be indicated, for example, by reference to a standard, by letter, by order note, or other means which allow the Zr + Ti limit.Aluminum content reported is calculated as remainder.Composition information provided by the Aluminum Association and is not for design.Key Words: UNS A97075; ISO AlZn5.5MgCu(A); Aluminium 7075-O; AA7075-OComponentWt. %Al87.1 - 91.4Cr0.18 - 0.28Cu1.2 - 2FeMax 0.5ComponentWt. %Mg2.1 - 2.9MnMax 0.3Other, eachMax 0.05Other, totalMax 0.15ComponentWt. %SiMax 0.4TiMax 0.2Zn5.1 - 6.1Material Notes: General 7075 characteristics and uses (from Alcoa): Very high strength material used for highly stressed structural parts. The T7351 temper offers improved stress-corrosion cracking resistance.Uses: Aircraft fittings, gears and shafts, fuse parts, meter shafts and gears, missile parts, regulating valve parts, worm gears, keys, aircraft, aerospace and defense applications.Data points with the AA note have been provided by the Aluminum Association, Inc. and are NOT FOR DESIGN.Click here to view available vendors for this material.Physical PropertiesMetricEnglishCommentsDensity2.81g/cc0.102lb/inAA; TypicalMechanical PropertiesHardness, Brinell6060AA; Typical; 500 g load; 10 mm ballHardness, Knoop8080Converted from Brinell Hardness ValueHardness, Vickers6868Converted from Brinell Hardness ValueUltimate Tensile Strength228MPa33000psiAA; TypicalTensile Yield Strength103MPa15000psiAA; TypicalElongation at Break16%16%AA; Typical; 1/2 in. (12.7 mm) DiameterElongation at Break17%17%AA; Typical; 1/16 in. (1.6 mm) ThicknessModulus of Elasticity71.7GPa10400ksiAA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.Poissons Ratio0.330.33Shear Modulus26.9GPa3900ksiShear Strength152MPa22000psiAA; TypicalElectrical PropertiesElectrical Resistivity3.8e-006ohm-cm3.8e-006ohm-cmThermal PropertiesCTE, linear 68F23.6m/m-C13.1in/in-FAA; Typical; Average over 68-212F range.CTE, linear 250C25.2m/m-C14in/in-FAverage over the range 20-300CSpecific Heat Capacity0.96J/g-C0.229BTU/lb-FThermal Conductivity173W/m-K1200BTU-in/hr-ft-FMelting Point477 - 635C890 - 1175FAA; Typical range based on typical composition for wrought products 1/4 inch thickness or greater. Homogenization may raise eutectic melting temperature 20-40F but usually does not eliminate eutectic melting.Solidus477C890FAA; TypicalLiquidus635C1175FAA; TypicalProcessing PropertiesAnnealing Temperature413C775FSolution Temperature466 - 482C870 - 900FAlclad Aluminum 2024-OSubcategory: 2000 Series Aluminum Alloy; Aluminum Alloy; Metal; Nonferrous MetalClose Analogs: Composition Notes: Composition for AA 2024 (not Alclad 2024 specifically).Aluminum content reported is calculated as remainder.Composition information provided by the Aluminum Association and is not for design.Key Words: Alclad 2024-O; Alclad 2024-OComponentWt. %Al90.7 - 94.7CrMax 0.1Cu3.8 - 4.9FeMax 0.5ComponentWt. %Mg1.2 - 1.8Mn0.3 - 0.9Other, eachMax 0.05Other, totalMax 0.15ComponentWt. %SiMax 0.5TiMax 0.15ZnMax 0.25Material Notes: Data points with the AA note have been provided by the Aluminum Association, Inc. and are NOT FOR DESIGN.Click here to view available vendors for this material.Physical PropertiesMetricEnglishCommentsDensity2.78g/cc0.1lb/inFor AA2024 (Not Alclad)Mechanical PropertiesUltimate Tensile Strength179MPa26000psiAA; TypicalTensile Yield Strength75.8MPa11000psiAA; TypicalElongation at Break20%20%AA; Typical; 1/16 in. (1.6 mm) ThicknessModulus of Elasticity73.1GPa10600ksiAA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.Shear Strength124MPa18000psiAA; TypicalProcessing PropertiesAnnealing Temperature413C775FSolution Temperature256C493FAluminum 2024-OSubcategory: 2000 Series Aluminum Alloy; Aluminum Alloy; Metal; Nonferrous MetalClose Analogs: Composition Notes: A Zr + Ti limit of 0.20 percent maximum may be used with this alloy designation for extruded and forged products only, but only when the supplier or producer and the purchaser have mutually so agreed. Agreement may be indicated, for example, by reference to a standard, by letter, by order note, or other means which allow the Zr + Ti limit.Aluminum content reported is calculated as remainder.Composition information provided by the Aluminum Association and is not for design.Key Words: Aluminium 2024-O; UNS A92024; ISO AlCu4Mg1; NF A-U4G1 (France); DIN AlCuMg2; AA2024-O, ASME SB211; CSA CG42 (Canada)ComponentWt. %Al90.7 - 94.7CrMax 0.1Cu3.8 - 4.9FeMax 0.5ComponentWt. %Mg1.2 - 1.8Mn0.3 - 0.9Other, eachMax 0.05Other, totalMax 0.15ComponentWt. %SiMax 0.5TiMax 0.15ZnMax 0.25Material Notes: General 2024 characteristics and uses (from Alcoa): Good machinability and surface finish capabilities. A high strength material of adequate workability. Has largely superceded 2017 for structural applications. Use of 2024-O not recommended unless subsequently heat treated.Uses: Aircraft fittings, gears and shafts, bolts, clock parts, computer parts, couplings, fuse parts, hydraulic valve bodies, missile parts, munitions, nuts, pistons, rectifier parts, worm gears, fastening devices, veterinary and orthopedic equipment, structures.Data points with the AA note have been provided by the Aluminum Association, Inc. and are NOT FOR DESIGN.Click here to view available vendors for this material.Physical PropertiesMetricEnglishCommentsDensity2.78g/cc0.1lb/inAA; TypicalMechanical PropertiesHardness, Brinell4747AA; Typical; 500 g load; 10 mm ballUltimate Tensile Strength186MPa27000psiAA; TypicalTensile Yield Strength75.8MPa11000psiAA; TypicalElongation at Break20%20%AA; Typical; 1/16 in. (1.6 mm) ThicknessElongation at Break22%22%AA; Typical; 1/2 in. (12.7 mm) DiameterModulus of Elasticity73.1GPa10600ksiAA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.Ultimate Bearing Strength345MPa50000psiEdge distance/pin diameter = 2.0Bearing Yield Strength131MPa19000psiEdge distance/pin diameter = 2.0Poissons Ratio0.330.33Fatigue Strength89.6MPa13000psiAA; 500,000,000 cycles completely reversed stress; RR Moore machine/specimenMachinability30%30%0-100 Scale of Aluminum AlloysShear Modulus28GPa4060ksiShear Strength124MPa18000psiAA; TypicalElectrical PropertiesElectrical Resistivity3.49e-006ohm-cm3.49e-006ohm-cmAA; Typical at 68FThermal PropertiesCTE, linear 68F23.2m/m-C12.9in/in-FAA; Typical; Average over 68-212F range.CTE, linear 250C24.7m/m-C13.7in/in-FAverage over the range 20-300CSpecific Heat Capacity0.875J/g-C0.209BTU/lb-FThermal Conductivity193W/m-K1340BTU-in/hr-ft-FAA; Typical at 77FMelting Point502 - 638C935 - 1180FAA; Typical range based on typical composition for wrought products 1/4 inch thickness or greater. Eutectic melting is not eliminated by homogenization.Solidus502C935FAA; TypicalLiquidus638C1180FAA; TypicalProcessing PropertiesAnnealing Temperature413C775FSolution Temperature256C493FAlclad Aluminum 2024-T4, T351Subcategory: 2000 Series Aluminum Alloy; Aluminum Alloy; Metal; Nonferrous MetalClose Analogs: Composition Notes: Composition for AA 2024 (not Alclad 2024).Aluminum content reported is calculated as remainder.Composition information provided by the Aluminum Association and is not for design.Key Words: Alclad 2024-T4, T351; Alclad 2024-T4, T351ComponentWt. %Al90.7 - 94.7CrMax 0.1Cu3.8 - 4.9FeMax 0.5ComponentWt. %Mg1.2 - 1.8Mn0.3 - 0.9Other, eachMax 0.05Other, totalMax 0.15ComponentWt. %SiMax 0.5TiMax 0.15ZnMax 0.25Material Notes: Data points with the AA note have been provided by the Aluminum Association, Inc. and are NOT FOR DESIGN.Click here to view available vendors for this material.Physical PropertiesMetricEnglishCommentsDensity2.78g/cc0.1lb/inFor AA2024 (Not Alclad)Mechanical PropertiesUltimate Tensile Strength441MPa64000psiAA; TypicalTensile Yield Strength290MPa42000psiAA; TypicalElongation at Break19%19%AA; Typical; 1/16 in. (1.6 mm) ThicknessModulus of Elasticity73.1GPa10600ksiAA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.Shear Strength276MPa40000psiAA; TypicalProcessing PropertiesAnnealing Temperature413C775FSolution Temperature256C493FAluminum 2024-T4; 2024-T351Subcategory: 2000 Series Aluminum Alloy; Aluminum Alloy; Metal; Nonferrous MetalClose Analogs: Composition Notes: A Zr + Ti limit of 0.20 percent maximum may be used with this alloy designation for extruded and forged products only, but only when the supplier or producer and the purchaser have mutually so agreed. Agreement may be indicated, for example, by reference to a standard, by letter, by order note, or other means which allow the Zr + Ti limit.Aluminum content reported is calculated as remainder.Composition information provided by the Aluminum Association and is not for design.Key Words: Aluminium 2024-T351; AA2024-T351, Aluminium 2024-T4; UNS A92024; ISO AlCu4Mg1; NF A-U4G1 (France); DIN AlCuMg2; AA2024-T4, ASME SB211; CSA CG42 (Cana