Alloy 2024

Chemical Composition Limits Others
Weight % Si Fe Cu Mn Mg Cr Zn Ti Each Total
Minimum - - 3.8 0.30 1.2 - - - - -
Maximum 0.50 0.50 4.9 0.9 1.8 0.10 0.25 0.15 0.05 0.15

Typical Physical Properties
Characteristic English Metric
Nominal Density (68 °F/20 °C) 0.100 lbs./in.3 2.77 Mg/m3
Melting Range 935 °F - 1180 °F 502 °C - 638 °C
Specific Heat (212 °F/100 °C) 0.209 BTU/lb. - °F 875 J/kg - °K
Coefficient of Thermal Expansion
Linear
68 °F-212 °F
20 °C-100 °C
12.7 micro in./in.-°F 22.9 micro m/m -°K
Volumetric
68 °F/20 °C
3.67 x 10-5in.3/in.3 -°F 66 x 10-6m3/m3 -°K
Thermal Conductivity (68°F/20°C) O Temper 110 BTU/ft. - hr. - °F 190 W/m - °K
T4,T351 69 BTU/ft. - hr. - °F 120 W/m - °K
T6,T851 88 BTU/ft. - hr. - °F 151 W/m - °K
Electrical Conductivity (68°F/20°C) Equal Volume O Temper 50% IACS
T4,T351 30% IACS
T6,T851 38% IACS
Equal Weight O Temper 160% IACS
T4,T351 96% IACS
T6,T851 122% IACS

Typical Mechanical Properties
  Tensile (.500" Dia. Specimen) Hardness Shear Fatigue* Modulus
Temper Yield Ultimate Elongation/4D
Brinell
500kg
10 mm
Ultimate Shearing Strength Endurance Limit R.R. Moore Type Modulus of Elasticity
KSI MPa KSI MPa %   KSI MPa KSI MPa KSI x 103 Gpa
0 11 76 27 186 22 47 18 124 13 90 10.6 73.1
T4,T351 47 324 68 469 19 120 41 283 20 138 10.6 73.1
T6 57 393 69 476 10 125 41 283 18 124 10.6 73.1
T851 65 448 70 482 7 128 43 296 18 124 10.6 73.1
*5 x 10E8 cycles of reversed stress
Comparative Characteristics
Temper Corrosion Resistance
Cold
Workability3
Machin-
ability3
Anodize
Response3
Braze-
ability4
Weldability4
General1 Stress2 Gas Arc Spot
T4,T351 D C C B C D C B B
T6 D B C B C D D C B
T851 D B D B C D D C B
1 Ratings A through E are relative ratings in decreasing order of merit, based on exposures to sodium chloride solution by intermittent spraying or immersion. Alloys with A and B ratings can be used in industrial and seacoast atmospheres without protection. Alloys with C, D and E ratings generally should be protected at least on faying surfaces.
2 Stress-corrosion cracking ratings are based on service experience and laboratory tests of specimens exposed to the 3.5% sodium chloride alternate immersion test.
A= No known instance of failure in service or in laboratory tests.
B= No known instance of failure in service; limited failures in laboratory tests of short transverse specimens.
C= Service failures with sustained tension stress acting in short transverse direction relative to grain structure; limited failures in laboratory tests of long transverse specimens.
D= Limited service failures with sustained longitudinal or long transverse

3 Ratings A through D for Workability (cold), A through E for Machinability and A through C for Anodize Response, are relative ratings in decreasing order of merit.
4 Ratings A through D for Weldability and Brazeability are relative ratings defined as follows:
A= Generally weldable by all commercial procedures and methods.
B= Weldable with special techniques or for specific applications that justify preliminary trails or testing to develop welding procedure and weld performance.
C= Limited weldability because of crack sensitivity or loss in resistance to corrosion and mechanical properties.
D= No commonly used welding methods have been developed.
Applicable Specifications  
Cold Finished Extruded
ASTM B211 ASTM B221
QQ-A-225/6 QQ-A-200/3
AMS 4112 AMS 4152
  AMS 4164
AMS 4120 AMS 4165

Alloy Description
2024 is heavily utilized in aircraft applications because it has good machining characteristics and higher strength than either 2014 and 2017. Through cold formability is considered fair, it is one of the most popular alloys for cold heading and thread rolling applications as a result of the superior grain structure that can be obtained. Corrosion resistance and anodizeablilty are only fair. It is also the basic alloy for cold finished square and rectangular bar. Again, this is because of its high strength and good machinability, which are essential for precision fittings and parts.

 
 
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