MakeItFrom.com
Menu (ESC)

ASTM A182 Grade F23 vs. 6012 Aluminum

ASTM A182 grade F23 belongs to the iron alloys classification, while 6012 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 6012 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 22
9.1 to 11
Fatigue Strength, MPa 320
55 to 100
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 74
26
Shear Strength, MPa 360
130 to 190
Tensile Strength: Ultimate (UTS), MPa 570
220 to 320
Tensile Strength: Yield (Proof), MPa 460
110 to 260

Thermal Properties

Latent Heat of Fusion, J/g 250
400
Maximum Temperature: Mechanical, °C 450
170
Melting Completion (Liquidus), °C 1500
640
Melting Onset (Solidus), °C 1450
570
Specific Heat Capacity, J/kg-K 470
890
Thermal Conductivity, W/m-K 41
160
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.8
45
Electrical Conductivity: Equal Weight (Specific), % IACS 8.9
140

Otherwise Unclassified Properties

Base Metal Price, % relative 7.0
9.5
Density, g/cm3 8.0
2.9
Embodied Carbon, kg CO2/kg material 2.5
8.2
Embodied Energy, MJ/kg 36
150
Embodied Water, L/kg 59
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
21 to 28
Resilience: Unit (Modulus of Resilience), kJ/m3 550
94 to 480
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 24
48
Strength to Weight: Axial, points 20
22 to 32
Strength to Weight: Bending, points 19
29 to 37
Thermal Diffusivity, mm2/s 11
62
Thermal Shock Resistance, points 17
10 to 14

Alloy Composition


Deprecated: Automatic conversion of false to array is deprecated in /home/public/compare.php on line 460
Aluminum (Al), % 0 to 0.030
92.2 to 98
Bismuth (Bi), % 0
0 to 0.7
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 0.3
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 93.2 to 96.2
0 to 0.5
Lead (Pb), % 0
0.4 to 2.0
Magnesium (Mg), % 0
0.6 to 1.2
Manganese (Mn), % 0.1 to 0.6
0.4 to 1.0
Molybdenum (Mo), % 0.050 to 0.3
0
Nickel (Ni), % 0 to 0.4
0
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
0.6 to 1.4
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0.0050 to 0.060
0 to 0.2
Tungsten (W), % 1.5 to 1.8
0
Vanadium (V), % 0.2 to 0.3
0
Zinc (Zn), % 0
0 to 0.3
Residuals, % 0
0 to 0.15