A medium strength aerospace aluminium alloy with strength, depending upon temperature.
See where AA Standards Grade 2024 T351 falls on the material property chart for Density against Elastic modulus in your materials selection and design process. Our Ashby charts are interactive with more technical data upon clicking. Sign up to get access to this premium feature for free.
Density
ρ2.77 - 3 g/cm³ at 23 °C
Dimensions
Durchmesser
Elongation
AElongation in 50 mm
Coefficient of thermal expansion
α2.32E-5 1/K at 20 °C
Melting point
Tm500 - 640 °C
Specific heat capacity
cp870 - 875 J/(kg·K) at 23 °C
Thermal conductivity
λ120 - 193 W/(m·K) at 23 °C
Electrical conductivity
σel1.70E+7 - 2.90E+7 S/m at 23 °C
Electrical resistivity
ρel3.45E-8 - 5.88E-8 Ω·m at 23 °C
Typical value
Element
Weight %
Comment
90.7 - 94.7 %
Balance
3.8 - 4.9 %
1.2 - 1.8 %
0.3 - 0.9 %
0 - 0.1 %
Application areas
Aerospace
Brazing
general: no brazing is known or developed
Corrosion properties
Stress corrosion cracking: Betriebsschäden in Gebieten mit Zugspannungen quer zur Kornstruktur, Eingeschränkte Schäden an Laborproben (T4,T3, T351, T3510, T3511), d (T6, T861, T81, T851, T8510, T8511), general: sufficient, in principle it should be protected
General machinability
General: poor (O), good to acceptable
Workability
general (condition): poor(T4, T3, T351, T3510, T3511, T6), not suitable (T361, T861, T81, T851, T8510, T8511)
This material data has been provided by MakeItFrom.com,ASM Handbook Volume 2 Properties and Selection: Nonferrous Alloys and Special-Purpose Materials,Matmatch,WroughtAl_ElectricalResistivity,Righton Blackburns,AluKey.