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ASTM A182 Grade F23 vs. 7010 Aluminum

ASTM A182 grade F23 belongs to the iron alloys classification, while 7010 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 ASTM A182 grade F23 and the bottom bar is 7010 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 22
3.9 to 6.8
Fatigue Strength, MPa 320
160 to 190
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 74
26
Shear Strength, MPa 360
300 to 340
Tensile Strength: Ultimate (UTS), MPa 570
520 to 590
Tensile Strength: Yield (Proof), MPa 460
410 to 540

Thermal Properties

Latent Heat of Fusion, J/g 250
380
Maximum Temperature: Mechanical, °C 450
200
Melting Completion (Liquidus), °C 1500
630
Melting Onset (Solidus), °C 1450
480
Specific Heat Capacity, J/kg-K 470
860
Thermal Conductivity, W/m-K 41
150
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.8
40
Electrical Conductivity: Equal Weight (Specific), % IACS 8.9
120

Otherwise Unclassified Properties

Base Metal Price, % relative 7.0
10
Density, g/cm3 8.0
3.0
Embodied Carbon, kg CO2/kg material 2.5
8.3
Embodied Energy, MJ/kg 36
150
Embodied Water, L/kg 59
1120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
22 to 33
Resilience: Unit (Modulus of Resilience), kJ/m3 550
1230 to 2130
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 24
45
Strength to Weight: Axial, points 20
47 to 54
Strength to Weight: Bending, points 19
47 to 52
Thermal Diffusivity, mm2/s 11
58
Thermal Shock Resistance, points 17
22 to 26

Alloy Composition


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Aluminum (Al), % 0 to 0.030
87.9 to 90.6
Boron (B), % 0.0010 to 0.0060
0
Carbon (C), % 0.040 to 0.1
0
Chromium (Cr), % 1.9 to 2.6
0 to 0.050
Copper (Cu), % 0
1.5 to 2.0
Iron (Fe), % 93.2 to 96.2
0 to 0.15
Magnesium (Mg), % 0
2.1 to 2.6
Manganese (Mn), % 0.1 to 0.6
0 to 0.1
Molybdenum (Mo), % 0.050 to 0.3
0
Nickel (Ni), % 0 to 0.4
0 to 0.050
Niobium (Nb), % 0.020 to 0.080
0
Nitrogen (N), % 0 to 0.015
0
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0 to 0.5
0 to 0.12
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0.0050 to 0.060
0 to 0.060
Tungsten (W), % 1.5 to 1.8
0
Vanadium (V), % 0.2 to 0.3
0
Zinc (Zn), % 0
5.7 to 6.7
Zirconium (Zr), % 0
0.1 to 0.16
Residuals, % 0
0 to 0.15