MakeItFrom.com
Menu (ESC)

2007 Aluminum vs. S34565 Stainless Steel

2007 aluminum belongs to the aluminum alloys classification, while S34565 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (5, 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 2007 aluminum and the bottom bar is S34565 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
210
Elongation at Break, % 5.6 to 8.0
39
Fatigue Strength, MPa 91 to 110
400
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
80
Shear Strength, MPa 220 to 250
610
Tensile Strength: Ultimate (UTS), MPa 370 to 420
900
Tensile Strength: Yield (Proof), MPa 240 to 270
470

Thermal Properties

Latent Heat of Fusion, J/g 390
310
Maximum Temperature: Mechanical, °C 190
1100
Melting Completion (Liquidus), °C 640
1420
Melting Onset (Solidus), °C 510
1380
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 130
12
Thermal Expansion, µm/m-K 23
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 47
1.9
Electrical Conductivity: Equal Weight (Specific), % IACS 140
2.1

Otherwise Unclassified Properties

Base Metal Price, % relative 11
28
Density, g/cm3 3.1
7.9
Embodied Carbon, kg CO2/kg material 8.0
5.3
Embodied Energy, MJ/kg 150
73
Embodied Water, L/kg 1130
210

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 21 to 26
300
Resilience: Unit (Modulus of Resilience), kJ/m3 390 to 530
540
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 44
25
Strength to Weight: Axial, points 33 to 38
32
Strength to Weight: Bending, points 37 to 40
26
Thermal Diffusivity, mm2/s 48
3.2
Thermal Shock Resistance, points 16 to 19
22

Alloy Composition

Aluminum (Al), % 87.5 to 95
0
Bismuth (Bi), % 0 to 0.2
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0 to 0.1
23 to 25
Copper (Cu), % 3.3 to 4.6
0
Iron (Fe), % 0 to 0.8
43.2 to 51.6
Lead (Pb), % 0.8 to 1.5
0
Magnesium (Mg), % 0.4 to 1.8
0
Manganese (Mn), % 0.5 to 1.0
5.0 to 7.0
Molybdenum (Mo), % 0
4.0 to 5.0
Nickel (Ni), % 0 to 0.2
16 to 18
Niobium (Nb), % 0
0 to 0.1
Nitrogen (N), % 0
0.4 to 0.6
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.8
0 to 1.0
Sulfur (S), % 0
0 to 0.010
Tin (Sn), % 0 to 0.2
0
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.8
0
Residuals, % 0 to 0.3
0