MakeItFrom.com
Menu (ESC)

ASTM A182 Grade F23 vs. 6016 Aluminum

ASTM A182 grade F23 belongs to the iron alloys classification, while 6016 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 F23 and the bottom bar is 6016 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 190
55 to 80
Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 22
11 to 27
Fatigue Strength, MPa 320
68 to 89
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 74
26
Shear Strength, MPa 360
130 to 170
Tensile Strength: Ultimate (UTS), MPa 570
200 to 280
Tensile Strength: Yield (Proof), MPa 460
110 to 210

Thermal Properties

Latent Heat of Fusion, J/g 250
410
Maximum Temperature: Mechanical, °C 450
160
Melting Completion (Liquidus), °C 1500
660
Melting Onset (Solidus), °C 1450
610
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 41
190 to 210
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.8
48 to 54
Electrical Conductivity: Equal Weight (Specific), % IACS 8.9
160 to 180

Otherwise Unclassified Properties

Base Metal Price, % relative 7.0
9.5
Density, g/cm3 8.0
2.7
Embodied Carbon, kg CO2/kg material 2.5
8.2
Embodied Energy, MJ/kg 36
150
Embodied Water, L/kg 59
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
29 to 47
Resilience: Unit (Modulus of Resilience), kJ/m3 550
82 to 340
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
51
Strength to Weight: Axial, points 20
21 to 29
Strength to Weight: Bending, points 19
29 to 35
Thermal Diffusivity, mm2/s 11
77 to 86
Thermal Shock Resistance, points 17
9.1 to 12

Alloy Composition


Deprecated: Automatic conversion of false to array is deprecated in /home/public/compare.php on line 460
Aluminum (Al), % 0 to 0.030
96.4 to 98.8
Boron (B), % 0.0010 to 0.0060
0
Carbon (C), % 0.040 to 0.1
0
Chromium (Cr), % 1.9 to 2.6
0 to 0.1
Copper (Cu), % 0
0 to 0.2
Iron (Fe), % 93.2 to 96.2
0 to 0.5
Magnesium (Mg), % 0
0.25 to 0.6
Manganese (Mn), % 0.1 to 0.6
0 to 0.2
Molybdenum (Mo), % 0.050 to 0.3
0
Nickel (Ni), % 0 to 0.4
0
Niobium (Nb), % 0.020 to 0.080
0
Nitrogen (N), % 0 to 0.015
0
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0 to 0.5
1.0 to 1.5
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0.0050 to 0.060
0 to 0.15
Tungsten (W), % 1.5 to 1.8
0
Vanadium (V), % 0.2 to 0.3
0
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15