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Aluminum 5083-O
Categories: Metal; Nonferrous Metal; Aluminum Alloy; 5000 Series Aluminum Alloy

Material Notes: This alloy has very good corrosion resistance (susceptible to deterioration after prolonged exposure to elevated temperatures) and moderate strength. Its weldability is a plus. It finds uses in transportation, pressure vessels, cryogenics, towers and drilling rigs, gas/oil piping, ordnance, and armor plate.

Data points with the AA note have been provided by the Aluminum Association, Inc. and are NOT FOR DESIGN.

Composition Notes:
Composition information provided by the Aluminum Association and is not for design.

Key Words: UNS A95083; ISO AlMg4.5Mn; Aluminium 5083-O; AA5083-O; Al5083-O
Vendors: No vendors are listed for this material. Please click here if you are a supplier and would like information on how to add your listing to this material.
 
Physical PropertiesOriginal ValueComments
Density 2.66 g/ccAA; Typical
 
Mechanical PropertiesOriginal ValueComments
Hardness, Brinell 77500 kg load with 10 mm ball. Calculated value.
Hardness, Knoop 100Converted from Brinell Hardness Value
Hardness, Vickers 87Converted from Brinell Hardness Value
Tensile Strength, Ultimate 42.0 ksiAA; Typical
 41.0 MPa
@Temperature 370 °C
 75.0 MPa
@Temperature 315 °C
 115 MPa
@Temperature 260 °C
 150 MPa
@Temperature 205 °C
 215 MPa
@Temperature 150 °C
 275 MPa
@Temperature 100 °C
 290 MPa
@Temperature -30.0 °C
 290 MPa
@Temperature 25.0 °C
 295 MPa
@Temperature -80.0 °C
 405 MPa
@Temperature -195 °C
 >= 250 MPa
@Thickness 177.8 - 203 mm
 >= 255 MPa
@Thickness 127.0 - 178 mm
 >= 260 MPa
@Thickness 76.23 - 127 mm
 270 - 345 MPa
@Thickness 38.13 - 76.2 mm
 275 - 350 MPa
@Thickness 1.30 - 38.1 mm
Tensile Strength, Yield 21.0 ksiAA; Typical
 >= 95.0 MPa
@Thickness 177.8 - 203 mm
 >= 105 MPa
@Thickness 127.0 - 178 mm
 >= 110 MPa
@Thickness 76.23 - 127 mm
 115 - 200 MPa
@Thickness 38.13 - 76.2 mm
 125 - 200 MPa
@Thickness 1.30 - 38.1 mm
 29.0 MPa
@Strain 0.2 %,
Temperature 370 °C
 50.0 MPa
@Strain 0.2 %,
Temperature 315 °C
 75.0 MPa
@Strain 0.2 %,
Temperature 260 °C
 115 MPa
@Strain 0.2 %,
Temperature 205 °C
 130 MPa
@Strain 0.2 %,
Temperature 150 °C
 145 MPa
@Strain 0.2 %,
Temperature -80.0 °C
 145 MPa
@Strain 0.2 %,
Temperature -30.0 °C
 145 MPa
@Strain 0.2 %,
Temperature 25.0 °C
 145 MPa
@Strain 0.2 %,
Temperature 100 °C
 165 MPa
@Strain 0.2 %,
Temperature -195 °C
Elongation at Break 25 %
@Temperature 25.0 °C
 27 %
@Temperature -30.0 °C
 30 %
@Temperature -80.0 °C
 36 %
@Temperature -195 °C
 36 %
@Temperature 100 °C
 50 %
@Temperature 150 °C
 60 %
@Temperature 205 °C
 80 %
@Temperature 260 °C
 110 %
@Temperature 315 °C
 130 %
@Temperature 370 °C
 >= 12 %
@Thickness 177.8 - 203 mm
 >= 14 %
@Thickness 127.0 - 178 mm
 14 - 16 %
@Thickness 76.23 - 127 mm
 >= 16 %
@Thickness 1.30 - 38.1 mm
 >= 16 %
@Thickness 38.13 - 76.2 mm
 22 %
@Diameter 12.7 mm
AA; Typical
Modulus of Elasticity 10300 ksiAA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.
Tensile Modulus 70.3 GPa
Compressive Modulus 71.7 GPa
Notched Tensile Strength 269 MPa2.5 cm width x 0.16 cm thick side-notched specimen, Kt = 17.
Ultimate Bearing Strength 552 MPaEdge distance/pin diameter = 2.0
Bearing Yield Strength 248 MPaEdge distance/pin diameter = 2.0
Poissons Ratio 0.33Estimated from trends in similar Al alloys.
Fatigue Strength 150 MPa
@# of Cycles 5.00e+8
unnotched R. R. Moore rotating beam
Machinability 30 %0-100 Scale of Aluminum Alloys
Shear Modulus 26.4 GPa
Shear Strength 25.0 ksiAA; Typical
 
Electrical PropertiesOriginal ValueComments
Electrical Resistivity 36.0 ohm-cir-mil/ft
@Temperature 20.0 °C
AA; Typical
 
Thermal PropertiesOriginal ValueComments
CTE, linear 13.2 µin/in-°F
@Temperature 20.0 - 100 °C
AA; Typical; average over range
 22.3 µm/m-°C
@Temperature -50.0 - 20.0 °C
 24.2 µm/m-°C
@Temperature 20.0 - 100 °C
 25.0 µm/m-°C
@Temperature 20.0 - 200 °C
 26.0 µm/m-°C
@Temperature 20.0 - 300 °C
Specific Heat Capacity 0.900 J/g-°C
Thermal Conductivity 810 BTU-in/hr-ft²-°FAA; Typical at 77°F
Melting Point 1095 - 1180 °FAA; Typical range based on typical composition for wrought products >= 1/4 in. thickness
Solidus 1095 °FAA; Typical
Liquidus 1180 °FAA; Typical
 
Processing PropertiesOriginal ValueComments
Annealing Temperature 775 °Fholding at temperature not required
Hot-Working Temperature 600 - 900 °F
 
Component Elements PropertiesOriginal ValueComments
Aluminum, Al 92.4 - 95.6 %As remainder
Chromium, Cr 0.05 - 0.25 %
Copper, Cu <= 0.10 %
Iron, Fe <= 0.40 %
Magnesium, Mg 4.0 - 4.9 %
Manganese, Mn 0.40 - 1.0 %
Other, each <= 0.05 %
Other, total <= 0.15 %
Silicon, Si <= 0.40 %
Titanium, Ti <= 0.15 %
Zinc, Zn <= 0.25 %

References for this datasheet.

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MA5083O / 9184

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