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Aluminum 5083-H116; 5083-H321
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: Aluminum 5083-H321; UNS A95083; ISO AlMg4.5Mn; Aluminium 5083-H116; Aluminium 5083-H321; AA5083-H116; Al5083-H116
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Physical PropertiesMetricEnglishComments
Density 2.66 g/cc0.0961 lb/in³AA; Typical
 
Mechanical PropertiesMetricEnglishComments
Hardness, Brinell 8585500 kg load with 10 mm ball. Calculated value.
Hardness, Knoop 109109Converted from Brinell Hardness Value
Hardness, Rockwell A 36.536.5Converted from Brinell Hardness Value
Hardness, Rockwell B 5353Converted from Brinell Hardness Value
Hardness, Vickers 9696Converted from Brinell Hardness Value
Tensile Strength, Ultimate 317 MPa46000 psiAA; Typical
 >= 285 MPa
@Thickness 38.13 - 76.2 mm
>= 41300 psi
@Thickness 1.501 - 3.00 in
 >= 305 MPa
@Thickness 1.60 - 38.1 mm
>= 44200 psi
@Thickness 0.0630 - 1.50 in
Tensile Strength, Yield 228 MPa33000 psiAA; Typical
 >= 200 MPa
@Thickness 38.13 - 76.2 mm
>= 29000 psi
@Thickness 1.501 - 3.00 in
 >= 215 MPa
@Thickness 1.60 - 38.1 mm
>= 31200 psi
@Thickness 0.0630 - 1.50 in
Elongation at Break  >= 12 %
@Thickness 1.60 - 38.1 mm
>= 12 %
@Thickness 0.0630 - 1.50 in
 >= 12 %
@Thickness 38.13 - 76.2 mm
>= 12 %
@Thickness 1.501 - 3.00 in
 16 %
@Diameter 12.7 mm
16 %
@Diameter 0.500 in
AA; Typical
Modulus of Elasticity 71.0 GPa10300 ksiAA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.
Tensile Modulus 70.3 GPa10200 ksi
Compressive Modulus 71.7 GPa10400 ksi
Poissons Ratio 0.330.33Estimated from trends in similar Al alloys.
Fatigue Strength 159 MPa
@# of Cycles 5.00e+8
23000 psi
@# of Cycles 5.00e+8
completely reversed stress; RR Moore machine/specimen
Fracture Toughness 43.0 MPa-m½39.1 ksi-in½KIC; TL orientation.
Machinability 30 %30 %0-100 Scale of Aluminum Alloys
Shear Modulus 26.4 GPa3830 ksi
Shear Strength 190 MPa27600 psiCalculated value.
 
Electrical PropertiesMetricEnglishComments
Electrical Resistivity 0.00000590 ohm-cm0.00000590 ohm-cm
 
Thermal PropertiesMetricEnglishComments
CTE, linear  22.3 µm/m-°C
@Temperature -50.0 - 20.0 °C
12.4 µin/in-°F
@Temperature -58.0 - 68.0 °F
 23.8 µm/m-°C
@Temperature 20.0 - 100 °C
13.2 µin/in-°F
@Temperature 68.0 - 212 °F
AA; Typical; average over range
 24.2 µm/m-°C
@Temperature 20.0 - 100 °C
13.4 µin/in-°F
@Temperature 68.0 - 212 °F
 25.0 µm/m-°C
@Temperature 20.0 - 200 °C
13.9 µin/in-°F
@Temperature 68.0 - 392 °F
 26.0 µm/m-°C
@Temperature 20.0 - 300 °C
14.4 µin/in-°F
@Temperature 68.0 - 572 °F
Specific Heat Capacity 0.900 J/g-°C0.215 BTU/lb-°F
Thermal Conductivity 117 W/m-K812 BTU-in/hr-ft²-°F
Melting Point 590.6 - 638 °C1095 - 1180 °FAA; Typical range based on typical composition for wrought products >= 1/4 in. thickness
Solidus 590.6 °C1095 °FAA; Typical
Liquidus 638 °C1180 °FAA; Typical
 
Processing PropertiesMetricEnglishComments
Annealing Temperature 413 °C775 °Fholding at temperature not required
Hot-Working Temperature 316 - 482 °C600 - 900 °F
 
Component Elements PropertiesMetricEnglishComments
Aluminum, Al 92.4 - 95.6 %92.4 - 95.6 %As remainder
Chromium, Cr 0.05 - 0.25 %0.05 - 0.25 %
Copper, Cu <= 0.10 %<= 0.10 %
Iron, Fe <= 0.40 %<= 0.40 %
Magnesium, Mg 4.0 - 4.9 %4.0 - 4.9 %
Manganese, Mn 0.40 - 1.0 %0.40 - 1.0 %
Other, each <= 0.05 %<= 0.05 %
Other, total <= 0.15 %<= 0.15 %
Silicon, Si <= 0.40 %<= 0.40 %
Titanium, Ti <= 0.15 %<= 0.15 %
Zinc, Zn <= 0.25 %<= 0.25 %

References for this datasheet.

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