AA Standards Grade 2024 T36

View suppliers (124)
Want to keep this datasheet? Save it now in your required format

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,MakeItFrom.com,WroughtAl_ElectricalResistivity.

"Typical" values were obtained via a literature search. "Predicted" values were imputed via artificial intelligence technology. While we have placed significant efforts in ensuring data accuracy, "typical" and "predicted" data should be considered indicative and verified by appropriate material testing. Please do contact us if additional information on the the predicted data method is required.
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.

Ashby charts

See where falls on the material property chart for against in your materials selection and design process. Our Ashby charts are interactive with more technical data upon clicking. Sign up to get access to this premium feature for free.

Properties

General

PropertyValueConditionRelated Standards

Density

2.78 g/cm³

Show Material materials with Density of 2.78 g/cm³

T36

AA Standards, ASTM B211

3.0 g/cm³

Show Material materials with Density of 3.0 g/cm³

T36

Mechanical

PropertyValueConditionRelated StandardsComment

Bending Fatigue Strength

125.0 MPa

Show Material materials with Bending Fatigue Strength of 125.0 MPa

T36

AA Standards

Elastic modulus

73.0 GPa

Show Material materials with Elastic modulus of 73.0 GPa

T36

AA Standards, ASTM B211

Elongation

10.0 %

Show Material materials with Elongation of 10.0 %

T36

AA Standards, ASTM B211

A50

12.0 %

Show Material materials with Elongation of 12.0 %

T36

13.0 %

Show Material materials with Elongation of 13.0 %

T36

AA Standards

A50

Hardness, Brinell

130.0 [-]

Show Material materials with Hardness, Brinell of 130.0 [-]

T36

AA Standards

Plane-Strain Fracture Toughnes

22.0 - 35.0 MPa·√m

Show Material materials with Plane-Strain Fracture Toughnes of 22.0 - 35.0 MPa·√m

Typical for Wrought 2000 Series Aluminium

Poisson's ratio

0.33 [-]

Show Material materials with Poisson's ratio of 0.33 [-]

Typical for Wrought 2000 Series Aluminium

Shear modulus

26.0 - 27.5 GPa

Show Material materials with Shear modulus of 26.0 - 27.5 GPa

Typical for Wrought 2000 Series Aluminium

Tensile strength

475.0 MPa

Show Material materials with Tensile strength of 475.0 MPa

T36

AA Standards, ASTM B211

495.0 MPa

Show Material materials with Tensile strength of 495.0 MPa

T36

AA Standards

550.0 MPa

Show Material materials with Tensile strength of 550.0 MPa

T36

Yield strength

360.0 MPa

Show Material materials with Yield strength of 360.0 MPa

T36

AA Standards, ASTM B211

RP02

395.0 MPa

Show Material materials with Yield strength of 395.0 MPa

T36

AA Standards

RP02

410.0 MPa

Show Material materials with Yield strength of 410.0 MPa

T36

Thermal

PropertyTemperatureValueConditionRelated Standards

Coefficient of thermal expansion

2.3e-05 1/K

Show Material materials with Coefficient of thermal expansion of 2.3e-05 1/K

T36

20 °C

2.3199999999999998e-05 1/K

Show Material materials with Coefficient of thermal expansion of 2.3199999999999998e-05 1/K

T36

AA Standards, ASTM B211

100 °C

2.3199999999999998e-05 1/K

Show Material materials with Coefficient of thermal expansion of 2.3199999999999998e-05 1/K

T36

AA Standards, ASTM B211

Melting point

500.0 °C

Show Material materials with Melting point of 500.0 °C

T36

505.0 - 635.0 °C

Show Material materials with Melting point of 505.0 - 635.0 °C

T36

AA Standards, ASTM B211

Specific heat capacity

870.0 J/(kg·K)

Show Material materials with Specific heat capacity of 870.0 J/(kg·K)

T36

Thermal conductivity

120.0 W/(m·K)

Show Material materials with Thermal conductivity of 120.0 W/(m·K)

T36

121.0 - 193.0 W/(m·K)

Show Material materials with Thermal conductivity of 121.0 - 193.0 W/(m·K)

T36

AA Standards, ASTM B211

Electrical

PropertyValueConditionRelated StandardsComment

Electrical conductivity

17000000.0 - 29000000.0 S/m

Show Material materials with Electrical conductivity of 17000000.0 - 29000000.0 S/m

T36

AA Standards, ASTM B211

Electrical resistivity

3.45e-08 - 5.88e-08 Ω·m

Show Material materials with Electrical resistivity of 3.45e-08 - 5.88e-08 Ω·m

T36

AA Standards, ASTM B211

5.7e-08 Ω·m

Show Material materials with Electrical resistivity of 5.7e-08 Ω·m

T36

Typical value

Chemical properties

PropertyValueConditionRelated Standards

Aluminium

90.7 - 94.7 %

Show Material materials with Aluminium of 90.7 - 94.7 %

T36

Chromium

0.1 %

Show Material materials with Chromium of 0.1 %

T36

AA Standards, ASTM B211

Copper

3.8 - 4.9 %

Show Material materials with Copper of 3.8 - 4.9 %

T36

AA Standards, ASTM B211

Iron

0.50 %

Show Material materials with Iron of 0.50 %

T36

AA Standards, ASTM B211

0.5 %

Show Material materials with Iron of 0.5 %

T36

Magnesium

1.2 - 1.8 %

Show Material materials with Magnesium of 1.2 - 1.8 %

T36

AA Standards, ASTM B211

Manganese

0.3 - 0.9 %

Show Material materials with Manganese of 0.3 - 0.9 %

T36

AA Standards, ASTM B211

Other

0.15 %

Show Material materials with Other of 0.15 %

T36

Silicon

0.5 %

Show Material materials with Silicon of 0.5 %

T36

AA Standards, ASTM B211

Titanium

0.15 %

Show Material materials with Titanium of 0.15 %

T36

AA Standards, ASTM B211

Zinc

0.25 %

Show Material materials with Zinc of 0.25 %

T36

AA Standards, ASTM B211

Zirconium

0.2 %

Show Material materials with Zirconium of 0.2 %

T36

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)