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7075-T6 Aluminum vs. Cold Finished AISI 316L

7075-T6 aluminum belongs to the aluminum alloys classification, while cold finished AISI 316L belongs to the iron alloys. There are 32 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 7075-T6 aluminum and the bottom bar is cold finished AISI 316L.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 150
210
Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 7.9
36
Fatigue Strength, MPa 160
350
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
78
Shear Strength, MPa 330
470
Tensile Strength: Ultimate (UTS), MPa 560
700
Tensile Strength: Yield (Proof), MPa 480
430

Thermal Properties

Latent Heat of Fusion, J/g 380
290
Maximum Temperature: Mechanical, °C 200
870
Melting Completion (Liquidus), °C 640
1400
Melting Onset (Solidus), °C 480
1380
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 130
15
Thermal Expansion, µm/m-K 23
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 98
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 10
19
Calomel Potential, mV -750
-50
Density, g/cm3 3.0
7.9
Embodied Carbon, kg CO2/kg material 8.3
3.9
Embodied Energy, MJ/kg 150
53
Embodied Water, L/kg 1120
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 42
220
Resilience: Unit (Modulus of Resilience), kJ/m3 1630
470
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 46
25
Strength to Weight: Axial, points 51
25
Strength to Weight: Bending, points 50
22
Thermal Diffusivity, mm2/s 50
4.1
Thermal Shock Resistance, points 24
15

Alloy Composition

Aluminum (Al), % 86.9 to 91.4
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0.18 to 0.28
16 to 18
Copper (Cu), % 1.2 to 2.0
0
Iron (Fe), % 0 to 0.5
62 to 72
Magnesium (Mg), % 2.1 to 2.9
0
Manganese (Mn), % 0 to 0.3
0 to 2.0
Molybdenum (Mo), % 0
2.0 to 3.0
Nickel (Ni), % 0
10 to 14
Nitrogen (N), % 0
0 to 0.1
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.4
0 to 0.75
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 5.1 to 6.1
0
Zirconium (Zr), % 0 to 0.25
0
Residuals, % 0 to 0.15
0