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ASTM A387 Grade 91 Class 2 vs. EN AC-45100 Aluminum

ASTM A387 grade 91 class 2 belongs to the iron alloys classification, while EN AC-45100 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-45100 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 200
97 to 130
Elastic (Young's, Tensile) Modulus, GPa 190
72
Elongation at Break, % 20
1.0 to 2.8
Fatigue Strength, MPa 330
82 to 99
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
27
Tensile Strength: Ultimate (UTS), MPa 670
300 to 360
Tensile Strength: Yield (Proof), MPa 470
210 to 320

Thermal Properties

Latent Heat of Fusion, J/g 270
470
Maximum Temperature: Mechanical, °C 600
170
Melting Completion (Liquidus), °C 1460
630
Melting Onset (Solidus), °C 1420
550
Specific Heat Capacity, J/kg-K 470
890
Thermal Conductivity, W/m-K 26
140
Thermal Expansion, µm/m-K 13
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 8.9
30
Electrical Conductivity: Equal Weight (Specific), % IACS 10
95

Otherwise Unclassified Properties

Base Metal Price, % relative 7.0
10
Density, g/cm3 7.8
2.8
Embodied Carbon, kg CO2/kg material 2.6
7.9
Embodied Energy, MJ/kg 37
150
Embodied Water, L/kg 88
1100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
3.5 to 7.6
Resilience: Unit (Modulus of Resilience), kJ/m3 580
290 to 710
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
49
Strength to Weight: Axial, points 24
30 to 35
Strength to Weight: Bending, points 22
35 to 39
Thermal Diffusivity, mm2/s 6.9
54
Thermal Shock Resistance, points 19
14 to 16

Alloy Composition

Aluminum (Al), % 0 to 0.020
88 to 92.8
Carbon (C), % 0.080 to 0.12
0
Chromium (Cr), % 8.0 to 9.5
0
Copper (Cu), % 0
2.6 to 3.6
Iron (Fe), % 87.3 to 90.3
0 to 0.6
Lead (Pb), % 0
0 to 0.1
Magnesium (Mg), % 0
0.15 to 0.45
Manganese (Mn), % 0.3 to 0.6
0 to 0.55
Molybdenum (Mo), % 0.85 to 1.1
0
Nickel (Ni), % 0 to 0.4
0 to 0.1
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
4.5 to 6.0
Sulfur (S), % 0 to 0.010
0
Tin (Sn), % 0
0 to 0.050
Titanium (Ti), % 0 to 0.010
0 to 0.25
Vanadium (V), % 0.18 to 0.25
0
Zinc (Zn), % 0
0 to 0.2
Zirconium (Zr), % 0 to 0.010
0
Residuals, % 0
0 to 0.15