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ASTM A387 Grade 91 Class 2 vs. 713.0 Aluminum

ASTM A387 grade 91 class 2 belongs to the iron alloys classification, while 713.0 aluminum belongs to the aluminum alloys. There are 31 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 713.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 200
74 to 75
Elastic (Young's, Tensile) Modulus, GPa 190
71
Elongation at Break, % 20
3.9 to 4.3
Fatigue Strength, MPa 330
63 to 120
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 75
27
Shear Strength, MPa 420
180
Tensile Strength: Ultimate (UTS), MPa 670
240 to 260
Tensile Strength: Yield (Proof), MPa 470
170

Thermal Properties

Latent Heat of Fusion, J/g 270
370
Maximum Temperature: Mechanical, °C 600
180
Melting Completion (Liquidus), °C 1460
630
Melting Onset (Solidus), °C 1420
610
Specific Heat Capacity, J/kg-K 470
860
Thermal Conductivity, W/m-K 26
150
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 8.9
35
Electrical Conductivity: Equal Weight (Specific), % IACS 10
100

Otherwise Unclassified Properties

Base Metal Price, % relative 7.0
9.5
Density, g/cm3 7.8
3.1
Embodied Carbon, kg CO2/kg material 2.6
7.8
Embodied Energy, MJ/kg 37
150
Embodied Water, L/kg 88
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
8.7 to 9.9
Resilience: Unit (Modulus of Resilience), kJ/m3 580
210 to 220
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
45
Strength to Weight: Axial, points 24
22 to 23
Strength to Weight: Bending, points 22
28 to 29
Thermal Diffusivity, mm2/s 6.9
57
Thermal Shock Resistance, points 19
10 to 11

Alloy Composition


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Aluminum (Al), % 0 to 0.020
87.6 to 92.4
Carbon (C), % 0.080 to 0.12
0
Chromium (Cr), % 8.0 to 9.5
0 to 0.35
Copper (Cu), % 0
0.4 to 1.0
Iron (Fe), % 87.3 to 90.3
0 to 1.1
Magnesium (Mg), % 0
0.2 to 0.5
Manganese (Mn), % 0.3 to 0.6
0 to 0.6
Molybdenum (Mo), % 0.85 to 1.1
0
Nickel (Ni), % 0 to 0.4
0 to 0.15
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
0 to 0.25
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0 to 0.010
0 to 0.25
Vanadium (V), % 0.18 to 0.25
0
Zinc (Zn), % 0
7.0 to 8.0
Zirconium (Zr), % 0 to 0.010
0
Residuals, % 0
0 to 0.25