MakeItFrom.com
Menu (ESC)

6151 Aluminum vs. EN 1.4597 Stainless Steel

6151 aluminum belongs to the aluminum alloys classification, while EN 1.4597 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, 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 6151 aluminum and the bottom bar is EN 1.4597 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 1.1 to 5.7
45
Fatigue Strength, MPa 80 to 100
300
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 190 to 200
470
Tensile Strength: Ultimate (UTS), MPa 330 to 340
680
Tensile Strength: Yield (Proof), MPa 270 to 280
330

Thermal Properties

Latent Heat of Fusion, J/g 410
290
Maximum Temperature: Mechanical, °C 170
860
Melting Completion (Liquidus), °C 650
1400
Melting Onset (Solidus), °C 590
1350
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 170
15
Thermal Expansion, µm/m-K 23
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 45
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 150
2.8

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
11
Density, g/cm3 2.7
7.7
Embodied Carbon, kg CO2/kg material 8.2
2.5
Embodied Energy, MJ/kg 150
36
Embodied Water, L/kg 1180
140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.5 to 18
250
Resilience: Unit (Modulus of Resilience), kJ/m3 520 to 580
280
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 34
25
Strength to Weight: Bending, points 39
22
Thermal Diffusivity, mm2/s 70
4.1
Thermal Shock Resistance, points 15
15

Alloy Composition

Aluminum (Al), % 95.6 to 98.8
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0.15 to 0.35
15 to 18
Copper (Cu), % 0 to 0.35
2.0 to 3.5
Iron (Fe), % 0 to 1.0
63 to 76.4
Magnesium (Mg), % 0.45 to 0.8
0
Manganese (Mn), % 0 to 0.2
6.5 to 9.0
Molybdenum (Mo), % 0
0 to 1.0
Nickel (Ni), % 0
0 to 3.0
Nitrogen (N), % 0
0.1 to 0.3
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0.6 to 1.2
0 to 2.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0