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
| Property | Temperature | Value | Condition | Related Standards |
|---|---|---|---|---|
Density | 20.0 °C | 2.77 g/cm³ | F44 | EN 573-3 |
Mechanical
| Property | Temperature | Value | Condition | Related Standards | Comment |
|---|---|---|---|---|---|
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
| Property | Temperature | Value | Condition | Related Standards | Comment |
|---|---|---|---|---|---|
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
| Property | Temperature | Value | Condition | Related Standards | Comment |
|---|---|---|---|---|---|
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
| Property | Value | Condition | Related 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
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- EN 573-3 AW-2024 F Aluminum Alloy – High Strength, Aircraft‑Grade Material
- EN 573-3 Grade AW-2024 H13 – High-Strength Aerospace Aluminum Alloy
- EN 573-3 AW-2024 H111 Aluminum Alloy – High Strength, Excellent Machinability
- EN 573-3 AW-2024 T3510 Aluminum Alloy – High Strength, Excellent Machinability
- EN 573-3 AW-2024 T3511 Aluminum Alloy: High Strength for Aircraft Applications
- EN 573-3 Grade AW-2024 T6 Aluminum – High Strength & Machinability for Aerospace
- EN 573-3 Grade AW‑2024 T651 – High‑Strength Aluminum Alloy for Aerospace