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7049 Aluminum vs. N08366 Stainless Steel

7049 aluminum belongs to the aluminum alloys classification, while N08366 stainless steel belongs to the iron alloys. There are 31 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 7049 aluminum and the bottom bar is N08366 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 140
180
Elastic (Young's, Tensile) Modulus, GPa 70
210
Elongation at Break, % 6.2 to 7.0
34
Fatigue Strength, MPa 160 to 170
190
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 27
80
Shear Strength, MPa 300 to 310
390
Tensile Strength: Ultimate (UTS), MPa 510 to 530
590
Tensile Strength: Yield (Proof), MPa 420 to 450
240

Thermal Properties

Latent Heat of Fusion, J/g 370
310
Maximum Temperature: Mechanical, °C 180
1100
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 480
1410
Specific Heat Capacity, J/kg-K 860
460
Thermal Conductivity, W/m-K 130
13
Thermal Expansion, µm/m-K 23
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 36
1.8
Electrical Conductivity: Equal Weight (Specific), % IACS 110
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 10
33
Density, g/cm3 3.1
8.1
Embodied Carbon, kg CO2/kg material 8.1
6.2
Embodied Energy, MJ/kg 140
84
Embodied Water, L/kg 1110
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 31 to 34
160
Resilience: Unit (Modulus of Resilience), kJ/m3 1270 to 1440
150
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
24
Strength to Weight: Axial, points 46 to 47
20
Strength to Weight: Bending, points 46 to 47
19
Thermal Diffusivity, mm2/s 51
3.4
Thermal Shock Resistance, points 22 to 23
13

Alloy Composition

Aluminum (Al), % 85.7 to 89.5
0
Carbon (C), % 0
0 to 0.035
Chromium (Cr), % 0.1 to 0.22
20 to 22
Copper (Cu), % 1.2 to 1.9
0
Iron (Fe), % 0 to 0.35
42.4 to 50.5
Magnesium (Mg), % 2.0 to 2.9
0
Manganese (Mn), % 0 to 0.2
0 to 2.0
Molybdenum (Mo), % 0
6.0 to 7.0
Nickel (Ni), % 0
23.5 to 25.5
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.25
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 7.2 to 8.2
0
Residuals, % 0 to 0.15
0