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ASTM A387 Grade 91 Class 2 vs. 5005A Aluminum

ASTM A387 grade 91 class 2 belongs to the iron alloys classification, while 5005A aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (1, 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 5005A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 200
29 to 64
Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 20
1.1 to 21
Fatigue Strength, MPa 330
38 to 82
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
26
Shear Strength, MPa 420
71 to 130
Tensile Strength: Ultimate (UTS), MPa 670
110 to 230
Tensile Strength: Yield (Proof), MPa 470
43 to 210

Thermal Properties

Latent Heat of Fusion, J/g 270
400
Maximum Temperature: Mechanical, °C 600
180
Melting Completion (Liquidus), °C 1460
660
Melting Onset (Solidus), °C 1420
630
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 26
200
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 8.9
52
Electrical Conductivity: Equal Weight (Specific), % IACS 10
170

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
8.3
Embodied Energy, MJ/kg 37
150
Embodied Water, L/kg 88
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
2.0 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 580
14 to 310
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 24
12 to 24
Strength to Weight: Bending, points 22
19 to 31
Thermal Diffusivity, mm2/s 6.9
82
Thermal Shock Resistance, points 19
5.0 to 10

Alloy Composition


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Aluminum (Al), % 0 to 0.020
97.5 to 99.3
Carbon (C), % 0.080 to 0.12
0
Chromium (Cr), % 8.0 to 9.5
0 to 0.1
Copper (Cu), % 0
0 to 0.050
Iron (Fe), % 87.3 to 90.3
0 to 0.45
Magnesium (Mg), % 0
0.7 to 1.1
Manganese (Mn), % 0.3 to 0.6
0 to 0.15
Molybdenum (Mo), % 0.85 to 1.1
0
Nickel (Ni), % 0 to 0.4
0
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 0.3
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0 to 0.010
0
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