Product Details, Specifications, and Technical Information
2024-T3511 aluminum is a high-strength alloy renowned for its excellent strength-to-weight ratio and fatigue resistance. The T3511 temper indicates that the material has been solution heat-treated, stress-relieved by stretching, and then straightened to meet standard tolerances. This process enhances its mechanical properties, making it ideal for aerospace applications such as aircraft structures, wing skins, and fuselage frames. While it offers good machinability, 2024-T3511 is more susceptible to corrosion compared to other aluminum alloys, necessitating appropriate protective measures

Dimension Name | Specification |
Legs | 1" x 1" |
Thickness | 0.094 |
Inside Radius | 0.188 |
Alloy | 2024 |
Temper | T3511 |
Production Method | Extruded |
DFAR | true |
Material | Aluminum |
Shape | Angle |
MTR Availability | Yes |
Domestic | true |
Brand | Aircraft Extrusion Co |
Ships | 1-3 Business Days |
Weight/Lineal Foot | ||
0.2279 pounds |
Please note that this data is to be used ONLY FOR REFERENCE, NOT FOR DESIGN, and by using it,you agree that any decisions you make regarding materials for your project are at your own discretion.
Mechanical Properties | |
Property | Value |
Density g/cm^3 | 3 |
Ultimate Tensile Strength KSI | 67 |
Yield Tensile Strength KSI | 46 |
Rockwell Hardness B Scale | 75 |
Brinell Hardness 500 kg load | 120 |
Melting Point °F | 935 - 1180 |
Elongation % in 2 in. | 9 |
Shear Strength KSI | 49 |
Machinability % | 70 |
Electrical Conductivity % IACS | 30 |
Chemistry Information: 2024 Aluminum | |
Element | Percentage |
Al | 93.5 |
Cr | 0.1 max |
Cu | 3.8 - 4.9 |
Mg | 1.2 - 1.8 |
Fe | 0.5 max |
Mn | 0.3 - 0.9 |
Si | 0.5 max |
Zn | 0.25 max |
Ti | 0.15 max |