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6005 Aluminum vs. ASTM A182 Grade F22V

6005 aluminum belongs to the aluminum alloys classification, while ASTM A182 grade F22V 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 6005 aluminum and the bottom bar is ASTM A182 grade F22V.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 90 to 95
210
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 9.5 to 17
21
Fatigue Strength, MPa 55 to 95
320
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
74
Shear Strength, MPa 120 to 210
420
Tensile Strength: Ultimate (UTS), MPa 190 to 310
670
Tensile Strength: Yield (Proof), MPa 100 to 280
460

Thermal Properties

Latent Heat of Fusion, J/g 410
250
Maximum Temperature: Mechanical, °C 160
460
Melting Completion (Liquidus), °C 650
1470
Melting Onset (Solidus), °C 610
1430
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 180 to 200
39
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 54
7.6
Electrical Conductivity: Equal Weight (Specific), % IACS 180
8.7

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
4.2
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 8.3
2.5
Embodied Energy, MJ/kg 150
35
Embodied Water, L/kg 1180
61

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 27 to 36
120
Resilience: Unit (Modulus of Resilience), kJ/m3 77 to 550
570
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 20 to 32
24
Strength to Weight: Bending, points 28 to 38
22
Thermal Diffusivity, mm2/s 74 to 83
11
Thermal Shock Resistance, points 8.6 to 14
19

Alloy Composition

Aluminum (Al), % 97.5 to 99
0
Boron (B), % 0
0 to 0.0020
Calcium (Ca), % 0
0 to 0.015
Carbon (C), % 0
0.11 to 0.15
Chromium (Cr), % 0 to 0.1
2.0 to 2.5
Copper (Cu), % 0 to 0.1
0 to 0.2
Iron (Fe), % 0 to 0.35
94.6 to 96.4
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.1
0.3 to 0.6
Molybdenum (Mo), % 0
0.9 to 1.1
Nickel (Ni), % 0
0 to 0.25
Niobium (Nb), % 0
0 to 0.070
Phosphorus (P), % 0
0 to 0.015
Silicon (Si), % 0.6 to 0.9
0 to 0.1
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.1
0 to 0.030
Vanadium (V), % 0
0.25 to 0.35
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0