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ASTM A182 Grade F36 vs. 6065 Aluminum

ASTM A182 grade F36 belongs to the iron alloys classification, while 6065 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (1, 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 ASTM A182 grade F36 and the bottom bar is 6065 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 17
4.5 to 11
Fatigue Strength, MPa 330
96 to 110
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 73
26
Shear Strength, MPa 440
190 to 230
Tensile Strength: Ultimate (UTS), MPa 710
310 to 400
Tensile Strength: Yield (Proof), MPa 490
270 to 380

Thermal Properties

Latent Heat of Fusion, J/g 250
400
Maximum Temperature: Mechanical, °C 410
180
Melting Completion (Liquidus), °C 1460
640
Melting Onset (Solidus), °C 1420
590
Specific Heat Capacity, J/kg-K 470
890
Thermal Conductivity, W/m-K 39
170
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.6
43
Electrical Conductivity: Equal Weight (Specific), % IACS 8.6
140

Otherwise Unclassified Properties

Base Metal Price, % relative 3.4
11
Density, g/cm3 7.9
2.8
Embodied Carbon, kg CO2/kg material 1.7
8.4
Embodied Energy, MJ/kg 22
150
Embodied Water, L/kg 53
1200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
17 to 34
Resilience: Unit (Modulus of Resilience), kJ/m3 650
540 to 1040
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
49
Strength to Weight: Axial, points 25
31 to 40
Strength to Weight: Bending, points 22
36 to 43
Thermal Diffusivity, mm2/s 10
67
Thermal Shock Resistance, points 21
14 to 18

Alloy Composition

Aluminum (Al), % 0 to 0.050
94.4 to 98.2
Bismuth (Bi), % 0
0.5 to 1.5
Carbon (C), % 0.1 to 0.17
0
Chromium (Cr), % 0 to 0.3
0 to 0.15
Copper (Cu), % 0.5 to 0.8
0.15 to 0.4
Iron (Fe), % 95 to 97.1
0 to 0.7
Lead (Pb), % 0
0 to 0.050
Magnesium (Mg), % 0
0.8 to 1.2
Manganese (Mn), % 0.8 to 1.2
0 to 0.15
Molybdenum (Mo), % 0.25 to 0.5
0
Nickel (Ni), % 1.0 to 1.3
0
Niobium (Nb), % 0.015 to 0.045
0
Nitrogen (N), % 0 to 0.020
0
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0.25 to 0.5
0.4 to 0.8
Sulfur (S), % 0 to 0.025
0
Titanium (Ti), % 0
0 to 0.1
Vanadium (V), % 0 to 0.020
0
Zinc (Zn), % 0
0 to 0.25
Zirconium (Zr), % 0
0 to 0.15
Residuals, % 0
0 to 0.15