MakeItFrom.com
Menu (ESC)

N08800 Stainless Steel vs. 7049A Aluminum

N08800 stainless steel belongs to the iron alloys classification, while 7049A aluminum belongs to the aluminum alloys. There are 30 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 N08800 stainless steel and the bottom bar is 7049A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
71
Elongation at Break, % 4.5 to 34
5.0 to 5.7
Fatigue Strength, MPa 150 to 390
180
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 77
27
Shear Strength, MPa 340 to 580
340 to 350
Tensile Strength: Ultimate (UTS), MPa 500 to 1000
580 to 590
Tensile Strength: Yield (Proof), MPa 190 to 830
500 to 530

Thermal Properties

Latent Heat of Fusion, J/g 300
370
Maximum Temperature: Mechanical, °C 1100
200
Melting Completion (Liquidus), °C 1390
640
Melting Onset (Solidus), °C 1360
430
Specific Heat Capacity, J/kg-K 480
850
Thermal Conductivity, W/m-K 12
130
Thermal Expansion, µm/m-K 14
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.7
40
Electrical Conductivity: Equal Weight (Specific), % IACS 1.9
120

Otherwise Unclassified Properties

Base Metal Price, % relative 30
10
Density, g/cm3 8.0
3.1
Embodied Carbon, kg CO2/kg material 5.3
8.2
Embodied Energy, MJ/kg 76
150
Embodied Water, L/kg 200
1100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 42 to 160
28 to 32
Resilience: Unit (Modulus of Resilience), kJ/m3 96 to 1740
1800 to 1990
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 24
44
Strength to Weight: Axial, points 18 to 35
52 to 53
Strength to Weight: Bending, points 18 to 28
50 to 51
Thermal Diffusivity, mm2/s 3.0
50
Thermal Shock Resistance, points 13 to 25
25

Alloy Composition


Deprecated: Automatic conversion of false to array is deprecated in /home/public/compare.php on line 460
Aluminum (Al), % 0.15 to 0.6
84.6 to 89.5
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 19 to 23
0.050 to 0.25
Copper (Cu), % 0 to 0.75
1.2 to 1.9
Iron (Fe), % 39.5 to 50.7
0 to 0.5
Magnesium (Mg), % 0
2.1 to 3.1
Manganese (Mn), % 0 to 1.5
0 to 0.5
Nickel (Ni), % 30 to 35
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 1.0
0 to 0.4
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0.15 to 0.6
0 to 0.25
Zinc (Zn), % 0
7.2 to 8.4
Zirconium (Zr), % 0
0 to 0.25
Residuals, % 0
0 to 0.15