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ASTM A182 Grade F92 vs. 242.0 Aluminum

ASTM A182 grade F92 belongs to the iron alloys classification, while 242.0 aluminum belongs to the aluminum alloys. There are 31 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 ASTM A182 grade F92 and the bottom bar is 242.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 240
70 to 110
Elastic (Young's, Tensile) Modulus, GPa 190
73
Elongation at Break, % 22
0.5 to 1.5
Fatigue Strength, MPa 360
55 to 110
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
27
Shear Strength, MPa 440
150 to 240
Tensile Strength: Ultimate (UTS), MPa 690
180 to 290
Tensile Strength: Yield (Proof), MPa 500
120 to 220

Thermal Properties

Latent Heat of Fusion, J/g 260
390
Maximum Temperature: Mechanical, °C 590
210
Melting Completion (Liquidus), °C 1490
640
Melting Onset (Solidus), °C 1450
530
Specific Heat Capacity, J/kg-K 470
870
Thermal Conductivity, W/m-K 26
130 to 170
Thermal Expansion, µm/m-K 13
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 9.3
33 to 44
Electrical Conductivity: Equal Weight (Specific), % IACS 10
96 to 130

Otherwise Unclassified Properties

Base Metal Price, % relative 11
12
Density, g/cm3 7.9
3.1
Embodied Carbon, kg CO2/kg material 2.8
8.3
Embodied Energy, MJ/kg 40
150
Embodied Water, L/kg 89
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140
1.3 to 3.4
Resilience: Unit (Modulus of Resilience), kJ/m3 650
110 to 340
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 24
45
Strength to Weight: Axial, points 24
16 to 26
Strength to Weight: Bending, points 22
23 to 32
Thermal Diffusivity, mm2/s 6.9
50 to 62
Thermal Shock Resistance, points 19
8.0 to 13

Alloy Composition

Aluminum (Al), % 0 to 0.020
88.4 to 93.6
Boron (B), % 0.0010 to 0.0060
0
Carbon (C), % 0.070 to 0.13
0
Chromium (Cr), % 8.5 to 9.5
0 to 0.25
Copper (Cu), % 0
3.5 to 4.5
Iron (Fe), % 85.8 to 89.1
0 to 1.0
Magnesium (Mg), % 0
1.2 to 1.8
Manganese (Mn), % 0.3 to 0.6
0 to 0.35
Molybdenum (Mo), % 0.3 to 0.6
0
Nickel (Ni), % 0 to 0.4
1.7 to 2.3
Niobium (Nb), % 0.040 to 0.090
0
Nitrogen (N), % 0.030 to 0.070
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.5
0 to 0.7
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0 to 0.010
0 to 0.25
Tungsten (W), % 1.5 to 2.0
0
Vanadium (V), % 0.15 to 0.25
0
Zinc (Zn), % 0
0 to 0.35
Zirconium (Zr), % 0 to 0.010
0
Residuals, % 0
0 to 0.15