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ASTM A387 Grade 91 Class 2 vs. EN AC-46400 Aluminum

ASTM A387 grade 91 class 2 belongs to the iron alloys classification, while EN AC-46400 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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 A387 grade 91 class 2 and the bottom bar is EN AC-46400 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 200
77 to 120
Elastic (Young's, Tensile) Modulus, GPa 190
72
Elongation at Break, % 20
1.1 to 1.7
Fatigue Strength, MPa 330
75 to 85
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
27
Tensile Strength: Ultimate (UTS), MPa 670
170 to 310
Tensile Strength: Yield (Proof), MPa 470
110 to 270

Thermal Properties

Latent Heat of Fusion, J/g 270
520
Maximum Temperature: Mechanical, °C 600
170
Melting Completion (Liquidus), °C 1460
610
Melting Onset (Solidus), °C 1420
570
Specific Heat Capacity, J/kg-K 470
890
Thermal Conductivity, W/m-K 26
130
Thermal Expansion, µm/m-K 13
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 8.9
33
Electrical Conductivity: Equal Weight (Specific), % IACS 10
110

Otherwise Unclassified Properties

Base Metal Price, % relative 7.0
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 2.6
7.8
Embodied Energy, MJ/kg 37
150
Embodied Water, L/kg 88
1070

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
1.7 to 4.9
Resilience: Unit (Modulus of Resilience), kJ/m3 580
82 to 500
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
52
Strength to Weight: Axial, points 24
18 to 32
Strength to Weight: Bending, points 22
26 to 38
Thermal Diffusivity, mm2/s 6.9
55
Thermal Shock Resistance, points 19
7.8 to 14

Alloy Composition

Aluminum (Al), % 0 to 0.020
85.4 to 90.5
Carbon (C), % 0.080 to 0.12
0
Chromium (Cr), % 8.0 to 9.5
0
Copper (Cu), % 0
0.8 to 1.3
Iron (Fe), % 87.3 to 90.3
0 to 0.8
Lead (Pb), % 0
0 to 0.1
Magnesium (Mg), % 0
0.25 to 0.65
Manganese (Mn), % 0.3 to 0.6
0.15 to 0.55
Molybdenum (Mo), % 0.85 to 1.1
0
Nickel (Ni), % 0 to 0.4
0 to 0.2
Niobium (Nb), % 0.060 to 0.1
0
Nitrogen (N), % 0.030 to 0.070
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0.2 to 0.5
8.3 to 9.7
Sulfur (S), % 0 to 0.010
0
Tin (Sn), % 0
0 to 0.1
Titanium (Ti), % 0 to 0.010
0 to 0.2
Vanadium (V), % 0.18 to 0.25
0
Zinc (Zn), % 0
0 to 0.8
Zirconium (Zr), % 0 to 0.010
0
Residuals, % 0
0 to 0.25