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705.0 Aluminum vs. EN 1.4913 Stainless Steel

705.0 aluminum belongs to the aluminum alloys classification, while EN 1.4913 stainless steel belongs to the iron alloys. There are 29 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 705.0 aluminum and the bottom bar is EN 1.4913 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 8.4 to 10
14 to 22
Fatigue Strength, MPa 63 to 98
320 to 480
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
75
Tensile Strength: Ultimate (UTS), MPa 240 to 260
870 to 980
Tensile Strength: Yield (Proof), MPa 130
480 to 850

Thermal Properties

Latent Heat of Fusion, J/g 390
270
Maximum Temperature: Mechanical, °C 180
700
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 610
1410
Specific Heat Capacity, J/kg-K 890
480
Thermal Conductivity, W/m-K 140
24
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 34
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 110
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.0
Density, g/cm3 2.8
7.8
Embodied Carbon, kg CO2/kg material 8.4
2.9
Embodied Energy, MJ/kg 150
41
Embodied Water, L/kg 1170
97

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 18 to 20
130 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 130
600 to 1860
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 49
25
Strength to Weight: Axial, points 24 to 26
31 to 35
Strength to Weight: Bending, points 31 to 32
26 to 28
Thermal Diffusivity, mm2/s 55
6.5
Thermal Shock Resistance, points 11
31 to 34

Alloy Composition

Aluminum (Al), % 92.3 to 98.6
0 to 0.020
Boron (B), % 0
0 to 0.0015
Carbon (C), % 0
0.17 to 0.23
Chromium (Cr), % 0 to 0.4
10 to 11.5
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.8
84.5 to 88.3
Magnesium (Mg), % 1.4 to 1.8
0
Manganese (Mn), % 0 to 0.6
0.4 to 0.9
Molybdenum (Mo), % 0
0.5 to 0.8
Nickel (Ni), % 0
0.2 to 0.6
Niobium (Nb), % 0
0.25 to 0.55
Nitrogen (N), % 0
0.050 to 0.1
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.2
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.25
0
Vanadium (V), % 0
0.1 to 0.3
Zinc (Zn), % 0 to 3.3
0
Residuals, % 0 to 0.15
0