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2024 T851 Aircraft Aluminum Sheet / High Strength Aluminium Flat Plate
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xProduct Details
| Enlongation | 23% | Tensile Strength | 66,000 PSI |
|---|---|---|---|
| Yield Strength | 58,000 PSI | Modulus Of Elasticity | 10500 Ksi |
| Coefficient Of Thermal Expansion @ 20.0 - 100 °C Temp | 23.2 µm/m-°C | 12.9 µin/in-°F | Thermal Conductivity | 121 W/m-K | 840 BTU-in/hr-ft²-°F |
| Density | 2.78 Grams Per Cubic Centimeters | ||
| Highlight | airplane aluminum sheets |
||
Product Description
High Strength And Excellent Fatigue Resistance 2024-T851 Aircraft Aluminum Sheets Plates
2024 is primarily alloyed with copper.
It also contains manganese and magnesium and can sometimes contain smaller amounts of silicon, iron, chromium, zinc and/or titanium.
It also contains manganese and magnesium and can sometimes contain smaller amounts of silicon, iron, chromium, zinc and/or titanium.
2024 alloy is often chosen for applications that require high strength
Characteristics On 2024-T851 Aluminum Sheets / Plates
Thermal Conductivity: 151 W/m-K | 1050 BTU-in/hr-ft²-°F
Coefficient of Thermal Expansion @ 20.0 - 100 °C Temp: 23.2 µm/m-°C | 12.9 µin/in-°F
Tensile Strength: 66000 psi
Yield Strength:58000 psi
Modulus of Elasticity: 10500 ksi
TYPICAL CHEMISTRY LIMITS:
| Element | Minimum % | Maximum % |
|---|---|---|
| Silicon | No Min | 0.5 |
| Iron | No Min | 0.5 |
| Copper | 3.8 | 4.9 |
| Manganese | 0.5 | 0.6 |
| Magnesium | 1.2 | 1.8 |
| Chromium | No Min | 0.1 |
| Zinc | No Min | 0.25 |
| Titanium | No Min | 0.15 |
| Other Elements | No Min | 0.05 each 0.15 in total |
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