AA 2024 T651 Aluminum Alloy – High Strength for Aerospace Applications
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.
Properties
General
| Property | Value | Condition |
|---|---|---|
Density | 2.78 g/cm³ | T651 |
3.0 g/cm³ | T651 |
Mechanical
| Property | Temperature | Value | Condition | Comment |
|---|---|---|---|---|
Elastic modulus | 73.0 GPa | T651 | ||
Elongation | -195 °C | 11 % | T651 | Elongation in 50 mm |
-80 °C | 10 % | T651 | Elongation in 50 mm | |
4.6 % | T651 | |||
0 °C | 10 % | T651 | Elongation in 50 mm | |
24 °C | 10 % | T651 | Elongation in 50 mm | |
100 °C | 10 % | T651 | Elongation in 50 mm | |
150 °C | 17 % | T651 | Elongation in 50 mm | |
205 °C | 27 % | T651 | Elongation in 50 mm | |
260 °C | 55 % | T651 | Elongation in 50 mm | |
315 °C | 75 % | T651 | Elongation in 50 mm | |
370 °C | 100 % | T651 | Elongation in 50 mm | |
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 | 28.0 GPa | T651 | ||
Tensile strength | -195 °C | 580 MPa | T651 | up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture |
-80 °C | 495 MPa | T651 | up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture | |
0 °C | 483 MPa | T651 | up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture | |
490.0 MPa | T651 | |||
24 °C | 475 MPa | T651 | up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture | |
100 °C | 448 MPa | T651 | up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture | |
150 °C | 310 MPa | T651 | up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture | |
205 °C | 180 MPa | T651 | up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture | |
260 °C | 75 MPa | T651 | up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture | |
315 °C | 52 MPa | T651 | up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture | |
370 °C | 35 MPa | T651 | up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture | |
Yield strength | -195 °C | 469 MPa | T651 | up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture, RP02 |
-80 °C | 407 MPa | T651 | up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture, RP02 | |
360.0 MPa | T651 | |||
0 °C | 400 MPa | T651 | up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture, RP02 | |
24 °C | 393 MPa | T651 | up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture, RP02 | |
100 °C | 372 MPa | T651 | up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture, RP02 | |
150 °C | 248 MPa | T651 | up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture, RP02 | |
205 °C | 131 MPa | T651 | up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture, RP02 | |
260 °C | 62 MPa | T651 | up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture, RP02 | |
315 °C | 41 MPa | T651 | up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture, RP02 | |
370 °C | 28 MPa | T651 | up to 10000 h at temperature, at 35 MPa/min to yield strength and then at strain rate of 5%/min to fracture, RP02 |
Thermal
| Property | Value | Condition |
|---|---|---|
Coefficient of thermal expansion | 2.3e-05 1/K | T651 |
Melting point | 500.0 °C | T651 |
Specific heat capacity | 870.0 J/(kg·K) | T651 |
Thermal conductivity | 120.0 W/(m·K) | T651 |
Electrical
| Property | Value | Comment |
|---|---|---|
Electrical conductivity | 18000000.0 - 30000000.0 S/m | Typical for Wrought 2000 Series Aluminium |
Electrical resistivity | 3.4e-08 - 6e-08 Ω·m | Typical for Wrought 2000 Series Aluminium |
Chemical properties
| Property | Value | Condition |
|---|---|---|
Aluminium | 90.7 - 94.7 % | T651 |
Chromium | 0.1 % | T651 |
Copper | 3.8 - 4.9 % | T651 |
Iron | 0.5 % | T651 |
Magnesium | 1.2 - 1.8 % | T651 |
Manganese | 0.3 - 0.9 % | T651 |
Other | 0.15 % | T651 |
Silicon | 0.5 % | T651 |
Titanium | 0.15 % | T651 |
Zinc | 0.25 % | T651 |
Zirconium | 0.2 % | T651 |
Technological properties
| Property | ||
|---|---|---|
| Workability | Moderate Workability | |
Metal
- JIS 2024 T4 Aluminum Alloy – High Strength, Machinability & Aerospace Applications
- JIS H4080 Grade 2024 O – Premium Aerospace-Grade Aluminum Alloy
- JIS H4040 Grade 2024 O Aluminum Alloy: High Strength & Machinability
- JIS H4000 Grade 2024 O – Premium 2024 Aluminium Alloy for Aerospace Applications
- ASTM B211 Grade 2024 O Aluminum – Superior Strength for Aerospace
- ASTM B241 Grade 2024-O Aluminum Alloy – Superior Strength for Aerospace Applications
- ASTM B211 2024‑T4 Aluminum Alloy – High Strength for Aerospace Applications
- ASTM B211 Grade 2024 T6 Aluminum: High-Strength, Aircraft-Grade Alloy
- AA 7475 T651: High-Toughness Aluminum Alloy for Versatile Applications
- EN 573-3 Grade AW‑2024 T651 – High‑Strength Aluminum Alloy for Aerospace