AA Standards Grade 2024 T3510

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Description

Aluminum AA 2024, known for its use in aircraft industry, is an alloy that offers excellent strength. When in the annealed condition it is readily formed and has good machinability. Though it has a relatively low level of corrosion resistance, it can be machined to a high finish.

Related Standards

Equivalent Materials

This material data has been provided by AluKey.

All metrics apply to room temperature unless otherwise stated. SI units used unless otherwise stated.
Equivalent standards are similar to one or more standards provided by the supplier. Some equivalent standards may be stricter whereas others may be outside the bounds of the original standard.

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Properties

General

PropertyValueConditionRelated Standards

Density

2.78 g/cm³

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T3510

AA Standards, ASTM B241

Mechanical

PropertyValueConditionRelated StandardsComment

Elastic modulus

73.0 GPa

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T3510

AA Standards, ASTM B241

Plane-Strain Fracture Toughnes

22.0 - 35.0 MPa·√m

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Typical for Wrought 2000 Series Aluminium

Poisson's ratio

0.33 [-]

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Typical for Wrought 2000 Series Aluminium

Shear modulus

26.0 - 27.5 GPa

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Typical for Wrought 2000 Series Aluminium

Tensile strength

395.0 MPa

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T3510

AA Standards, ASTM B241

415.0 MPa

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T3510

AA Standards, ASTM B241

450.0 MPa

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T3510

AA Standards, ASTM B241

470.0 MPa

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T3510

AA Standards, ASTM B241

Thermal

PropertyTemperatureValueConditionRelated StandardsComment

Coefficient of thermal expansion

20 °C

2.3199999999999998e-05 1/K

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T3510

AA Standards, ASTM B241

100 °C

2.3199999999999998e-05 1/K

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T3510

AA Standards, ASTM B241

Melting point

505.0 - 635.0 °C

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T3510

AA Standards, ASTM B241

Specific heat capacity

816.0 - 963.0 J/(kg·K)

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Typical for Wrought 2000 Series Aluminium

Thermal conductivity

121.0 - 193.0 W/(m·K)

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T3510

AA Standards, ASTM B241

Electrical

PropertyValueConditionRelated Standards

Electrical conductivity

17000000.0 - 29000000.0 S/m

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T3510

AA Standards, ASTM B241

Electrical resistivity

3.45e-08 - 5.88e-08 Ω·m

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T3510

AA Standards, ASTM B241

Chemical properties

PropertyValueConditionRelated Standards

Chromium

0.1 %

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T3510

AA Standards, ASTM B241

Copper

3.8 - 4.9 %

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T3510

AA Standards, ASTM B241

Iron

0.50 %

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T3510

AA Standards, ASTM B241

Magnesium

1.2 - 1.8 %

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T3510

AA Standards, ASTM B241

Manganese

0.3 - 0.9 %

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T3510

AA Standards, ASTM B241

Silicon

0.5 %

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T3510

AA Standards, ASTM B241

Titanium

0.15 %

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T3510

AA Standards, ASTM B241

Zinc

0.25 %

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T3510

AA Standards, ASTM B241

Technological properties

Property
Brazing

general: no brazing is known or developed

Corrosion properties

Stress corrosion cracking: Betriebsschäden in Gebieten mit Zugspannungen quer zur Kornstruktur, Eingeschränkte Schäden an Laborproben (T4,T3, T351, T3510, T3511), d (T6, T861, T81, T851, T8510, T8511), general: sufficient, in principle it should be protected

General machinability

General: poor (O), good to acceptable

Workability

general (condition): poor(T4, T3, T351, T3510, T3511, T6), not suitable (T361, T861, T81, T851, T8510, T8511)