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7178 Aluminum vs. EN 1.4905 Stainless Steel

7178 aluminum belongs to the aluminum alloys classification, while EN 1.4905 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 7178 aluminum and the bottom bar is EN 1.4905 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 4.5 to 12
19
Fatigue Strength, MPa 120 to 210
330
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 27
76
Shear Strength, MPa 140 to 380
460
Tensile Strength: Ultimate (UTS), MPa 240 to 640
740
Tensile Strength: Yield (Proof), MPa 120 to 560
510

Thermal Properties

Latent Heat of Fusion, J/g 370
270
Maximum Temperature: Mechanical, °C 180
660
Melting Completion (Liquidus), °C 630
1480
Melting Onset (Solidus), °C 480
1440
Specific Heat Capacity, J/kg-K 860
470
Thermal Conductivity, W/m-K 130
26
Thermal Expansion, µm/m-K 23
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 31
3.7
Electrical Conductivity: Equal Weight (Specific), % IACS 91
4.2

Otherwise Unclassified Properties

Base Metal Price, % relative 10
9.5
Density, g/cm3 3.1
7.9
Embodied Carbon, kg CO2/kg material 8.2
2.8
Embodied Energy, MJ/kg 150
40
Embodied Water, L/kg 1110
90

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24 to 52
130
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 2220
680
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
24
Strength to Weight: Axial, points 21 to 58
26
Strength to Weight: Bending, points 28 to 54
23
Thermal Diffusivity, mm2/s 47
7.0
Thermal Shock Resistance, points 10 to 28
25

Alloy Composition


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Aluminum (Al), % 85.4 to 89.5
0 to 0.040
Boron (B), % 0
0.00050 to 0.0050
Carbon (C), % 0
0.090 to 0.13
Chromium (Cr), % 0.18 to 0.28
8.5 to 9.5
Copper (Cu), % 1.6 to 2.4
0
Iron (Fe), % 0 to 0.5
86.2 to 88.8
Magnesium (Mg), % 2.4 to 3.1
0
Manganese (Mn), % 0 to 0.3
0.3 to 0.6
Molybdenum (Mo), % 0
0.9 to 1.1
Nickel (Ni), % 0
0.1 to 0.4
Niobium (Nb), % 0
0.060 to 0.1
Nitrogen (N), % 0
0.050 to 0.090
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.4
0.1 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.2
0
Tungsten (W), % 0
0.9 to 1.1
Vanadium (V), % 0
0.18 to 0.25
Zinc (Zn), % 6.3 to 7.3
0
Residuals, % 0 to 0.15
0