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7005 Aluminum vs. ASTM A182 Grade F12 Class 2

7005 aluminum belongs to the aluminum alloys classification, while ASTM A182 grade F12 class 2 belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is 7005 aluminum and the bottom bar is ASTM A182 grade F12 class 2.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 10 to 20
22
Fatigue Strength, MPa 100 to 190
220
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 120 to 230
340
Tensile Strength: Ultimate (UTS), MPa 200 to 400
540
Tensile Strength: Yield (Proof), MPa 95 to 350
310

Thermal Properties

Latent Heat of Fusion, J/g 380
250
Maximum Temperature: Mechanical, °C 200
430
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 610
1420
Specific Heat Capacity, J/kg-K 880
470
Thermal Conductivity, W/m-K 140 to 170
43
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35 to 43
7.3
Electrical Conductivity: Equal Weight (Specific), % IACS 110 to 130
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
2.8
Density, g/cm3 2.9
7.8
Embodied Carbon, kg CO2/kg material 8.3
1.6
Embodied Energy, MJ/kg 150
21
Embodied Water, L/kg 1150
52

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 32 to 57
100
Resilience: Unit (Modulus of Resilience), kJ/m3 65 to 850
260
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 47
24
Strength to Weight: Axial, points 19 to 38
19
Strength to Weight: Bending, points 26 to 41
19
Thermal Diffusivity, mm2/s 54 to 65
12
Thermal Shock Resistance, points 8.7 to 18
16

Alloy Composition

Aluminum (Al), % 91 to 94.7
0
Carbon (C), % 0
0.1 to 0.2
Chromium (Cr), % 0.060 to 0.2
0.8 to 1.3
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.4
96.4 to 98.3
Magnesium (Mg), % 1.0 to 1.8
0
Manganese (Mn), % 0.2 to 0.7
0.3 to 0.8
Molybdenum (Mo), % 0
0.44 to 0.65
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.35
0.1 to 0.6
Sulfur (S), % 0
0 to 0.040
Titanium (Ti), % 0.010 to 0.060
0
Zinc (Zn), % 4.0 to 5.0
0
Zirconium (Zr), % 0.080 to 0.2
0
Residuals, % 0 to 0.15
0