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EN 573-3 AW-2024 F44 Aluminum Alloy – Aircraft-Grade Strength & Machinability

Aluminum EN AW-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.

Properties

General

PropertyTemperatureValueConditionRelated Standards

Density

20.0 °C

2.77 g/cm³

F44

EN 573-3

Mechanical

PropertyTemperatureValueConditionRelated StandardsComment

Elastic modulus

20.0 °C

70.0 - 74.5 GPa

F44

EN 573-3

Elongation

-196.0 °C

19.0 %

F44

EN 573-3

-80.0 °C

19.0 %

F44

EN 573-3

-28.0 °C

19.0 %

F44

EN 573-3

20.0 °C

19.0 %

F44

EN 573-3

100.0 °C

19.0 %

F44

EN 573-3

150.0 °C

17.0 %

F44

EN 573-3

200.0 °C

27.0 %

F44

EN 573-3

260.0 °C

55.0 %

F44

EN 573-3

315.0 °C

75.0 %

F44

EN 573-3

370.0 °C

100.0 %

F44

EN 573-3

Plane-Strain Fracture Toughnes

22.0 - 35.0 MPa·√m

Typical for Wrought 2000 Series Aluminium

Poisson's ratio

0.33 [-]

Typical for Wrought 2000 Series Aluminium

Shear modulus

20.0 °C

27.0 - 28.0 GPa

F44

EN 573-3

Tensile strength

-196.0 °C

580.0 MPa

F44

EN 573-3

-80.0 °C

490.0 MPa

F44

EN 573-3

-28.0 °C

475.0 MPa

F44

EN 573-3

20.0 °C

470.0 MPa

F44

EN 573-3

100.0 °C

435.0 MPa

F44

EN 573-3

150.0 °C

310.0 MPa

F44

EN 573-3

200.0 °C

180.0 MPa

F44

EN 573-3

260.0 °C

75.0 MPa

F44

EN 573-3

315.0 °C

50.0 MPa

F44

EN 573-3

370.0 °C

35.0 MPa

F44

EN 573-3

Thermal

PropertyTemperatureValueConditionRelated StandardsComment

Coefficient of thermal expansion

1.6e-05 - 2.4e-05 1/K

Typical for Wrought 2000 Series Aluminium

Melting point

500.0 - 650.0 °C

Typical for Wrought 2000 Series Aluminium

Specific heat capacity

20.0 °C

875.0 J/(kg·K)

F44

EN 573-3

Thermal conductivity

20.0 °C

130.0 - 150.0 W/(m·K)

F44

EN 573-3

Electrical

PropertyTemperatureValueConditionRelated StandardsComment

Electrical conductivity

20.0 °C

18000000.0 - 21000000.0 S/m

F44

EN 573-3

Electrical resistivity

3.4e-08 - 6e-08 Ω·m

Typical for Wrought 2000 Series Aluminium

Chemical properties

PropertyValueConditionRelated Standards

Chromium

0.1

F44

EN 573-3

Copper

3.8 - 4.9 %

F44

EN 573-3

Iron

0.5

F44

EN 573-3

Magnesium

1.2 - 1.8 %

F44

EN 573-3

Manganese

0.3 - 0.9 %

F44

EN 573-3

Silicon

0.5

F44

EN 573-3

Titanium

0.15

F44

EN 573-3

Zinc

0.25

F44

EN 573-3

Technological properties

Property
Workability

Moderate Workability


Metal

  1. EN 573-3 AW-2024 H18 Aluminum Alloy – High Strength & Machinability for Aerospace Applications
  2. EN 573-3 Grade AW-2024 O3 – High-Strength Aluminum Alloy for Aerospace
  3. EN 573-3 Grade AW‑2024 T4510 – Premium Aircraft‑Grade Aluminum Alloy
  4. EN 573-3 AW-2024 F Aluminum Alloy – High Strength, Aircraft‑Grade Material
  5. EN 573-3 Grade AW-2024 H13 – High-Strength Aerospace Aluminum Alloy
  6. EN 573-3 AW-2024 H111 Aluminum Alloy – High Strength, Excellent Machinability
  7. EN 573-3 AW-2024 T3510 Aluminum Alloy – High Strength, Excellent Machinability
  8. EN 573-3 AW-2024 T3511 Aluminum Alloy: High Strength for Aircraft Applications
  9. EN 573-3 Grade AW-2024 T6 Aluminum – High Strength & Machinability for Aerospace
  10. EN 573-3 Grade AW‑2024 T651 – High‑Strength Aluminum Alloy for Aerospace