MakeItFrom.com
Menu (ESC)

ASTM A387 Grade 21 Steel vs. 2014A Aluminum

ASTM A387 grade 21 steel belongs to the iron alloys classification, while 2014A 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 21 steel and the bottom bar is 2014A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
72
Elongation at Break, % 21
6.2 to 16
Fatigue Strength, MPa 160 to 250
93 to 150
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 74
27
Shear Strength, MPa 310 to 370
130 to 290
Tensile Strength: Ultimate (UTS), MPa 500 to 590
210 to 490
Tensile Strength: Yield (Proof), MPa 230 to 350
110 to 430

Thermal Properties

Latent Heat of Fusion, J/g 260
400
Maximum Temperature: Mechanical, °C 480
210
Melting Completion (Liquidus), °C 1470
640
Melting Onset (Solidus), °C 1430
510
Specific Heat Capacity, J/kg-K 470
870
Thermal Conductivity, W/m-K 41
150
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.6
37
Electrical Conductivity: Equal Weight (Specific), % IACS 8.8
110

Otherwise Unclassified Properties

Base Metal Price, % relative 4.1
11
Density, g/cm3 7.9
3.0
Embodied Carbon, kg CO2/kg material 1.8
8.1
Embodied Energy, MJ/kg 23
150
Embodied Water, L/kg 62
1140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 84 to 110
24 to 49
Resilience: Unit (Modulus of Resilience), kJ/m3 140 to 320
85 to 1300
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 24
46
Strength to Weight: Axial, points 18 to 21
19 to 45
Strength to Weight: Bending, points 18 to 20
26 to 46
Thermal Diffusivity, mm2/s 11
55
Thermal Shock Resistance, points 14 to 17
9.0 to 22

Alloy Composition

Aluminum (Al), % 0
90.8 to 95
Carbon (C), % 0.050 to 0.15
0
Chromium (Cr), % 2.8 to 3.3
0 to 0.1
Copper (Cu), % 0
3.9 to 5.0
Iron (Fe), % 94.4 to 96
0 to 0.5
Magnesium (Mg), % 0
0.2 to 0.8
Manganese (Mn), % 0.3 to 0.6
0.4 to 1.2
Molybdenum (Mo), % 0.9 to 1.1
0
Nickel (Ni), % 0
0 to 0.1
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 0.5
0.5 to 0.9
Sulfur (S), % 0 to 0.025
0
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.25
Zirconium (Zr), % 0
0 to 0.2
Residuals, % 0
0 to 0.15

Comparable Variants