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N08800 Stainless Steel vs. 4032 Aluminum

N08800 stainless steel belongs to the iron alloys classification, while 4032 aluminum belongs to the aluminum 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 N08800 stainless steel and the bottom bar is 4032 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
73
Elongation at Break, % 4.5 to 34
6.7
Fatigue Strength, MPa 150 to 390
110
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
28
Shear Strength, MPa 340 to 580
260
Tensile Strength: Ultimate (UTS), MPa 500 to 1000
390
Tensile Strength: Yield (Proof), MPa 190 to 830
320

Thermal Properties

Latent Heat of Fusion, J/g 300
570
Maximum Temperature: Mechanical, °C 1100
180
Melting Completion (Liquidus), °C 1390
570
Melting Onset (Solidus), °C 1360
530
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 12
140
Thermal Expansion, µm/m-K 14
19

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.7
34
Electrical Conductivity: Equal Weight (Specific), % IACS 1.9
120

Otherwise Unclassified Properties

Base Metal Price, % relative 30
10
Density, g/cm3 8.0
2.6
Embodied Carbon, kg CO2/kg material 5.3
7.8
Embodied Energy, MJ/kg 76
140
Embodied Water, L/kg 200
1030

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 42 to 160
25
Resilience: Unit (Modulus of Resilience), kJ/m3 96 to 1740
700
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 24
53
Strength to Weight: Axial, points 18 to 35
41
Strength to Weight: Bending, points 18 to 28
45
Thermal Diffusivity, mm2/s 3.0
59
Thermal Shock Resistance, points 13 to 25
20

Alloy Composition

Aluminum (Al), % 0.15 to 0.6
81.1 to 87.2
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 19 to 23
0 to 0.1
Copper (Cu), % 0 to 0.75
0.5 to 1.3
Iron (Fe), % 39.5 to 50.7
0 to 1.0
Magnesium (Mg), % 0
0.8 to 1.3
Manganese (Mn), % 0 to 1.5
0
Nickel (Ni), % 30 to 35
0.5 to 1.3
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
11 to 13.5
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0.15 to 0.6
0
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15