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Aluminum 5052-H32
Categories: Metal; Nonferrous Metal; Aluminum Alloy; 5000 Series Aluminum Alloy
Material Notes: This alloy has good workability, very good corrosion resistance, high fatigue strength, weldability, and moderate strength. This leads to its use in aircraft fuel/oil lines, fuel tanks, other transportation areas, sheet metal work, appliances and lighting, wire, and rivets.

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 A95052; ISO AlMg2.5; Aluminium 5052-H32; AA5052-H32; Al5052-H32
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Physical PropertiesOriginal ValueComments
Density 2.68 g/ccAA; Typical
 
Mechanical PropertiesOriginal ValueComments
Hardness, Brinell 60AA; Typical; 500 g load; 10 mm ball
Hardness, Knoop 83Converted from Brinell Hardness Value
Hardness, Vickers 68Converted from Brinell Hardness Value
Tensile Strength, Ultimate 33.0 ksiAA; Typical
Tensile Strength, Yield 28.0 ksiAA; Typical
Elongation at Break 12 %
@Thickness 1.59 mm		AA; Typical
 18 %
@Diameter 12.7 mm		AA; Typical
Modulus of Elasticity 10200 ksiAA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.
Poissons Ratio 0.33
Fatigue Strength 17000 psi
@# of Cycles 5.00e+8 		completely reversed stress; RR Moore machine/specimen
Shear Modulus 25.9 GPa
Shear Strength 20.0 ksiAA; Typical
 
Electrical PropertiesOriginal ValueComments
Electrical Resistivity 30.0 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
 22.1 µm/m-°C
@Temperature -50.0 - 20.0 °C
 24.8 µm/m-°C
@Temperature 20.0 - 200 °C
 25.7 µm/m-°C
@Temperature 20.0 - 300 °C
Specific Heat Capacity 0.880 J/g-°CEstimated from trends in similar Al alloys.
Thermal Conductivity 960 BTU-in/hr-ft²-°FAA; Typical at 77°F
Melting Point 1125 - 1200 °FAA; Typical range based on typical composition for wrought products >= 1/4 in. thickness
Solidus 1125 °FAA; Typical
Liquidus 1200 °FAA; Typical
 
Processing PropertiesOriginal ValueComments
Annealing Temperature 650 °Fholding at temperature not required
Hot-Working Temperature 500 - 950 °F
 
Component Elements PropertiesOriginal ValueComments
Aluminum, Al 95.7 - 97.7 %As remainder
Chromium, Cr 0.15 - 0.35 %
Copper, Cu <= 0.10 %
Iron, Fe <= 0.40 %
Magnesium, Mg 2.2 - 2.8 %
Manganese, Mn <= 0.10 %
Other, each <= 0.05 %
Other, total <= 0.15 %
Silicon, Si <= 0.25 %
Zinc, Zn <= 0.10 %

References for this datasheet.

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MA5052H32 / 9155




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