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ASTM A182 Grade F92 vs. 1235 Aluminum

ASTM A182 grade F92 belongs to the iron alloys classification, while 1235 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 ASTM A182 grade F92 and the bottom bar is 1235 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 22
28 to 34
Fatigue Strength, MPa 360
23 to 58
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Shear Strength, MPa 440
52 to 56
Tensile Strength: Ultimate (UTS), MPa 690
80 to 84
Tensile Strength: Yield (Proof), MPa 500
23 to 57

Thermal Properties

Latent Heat of Fusion, J/g 260
400
Maximum Temperature: Mechanical, °C 590
170
Melting Completion (Liquidus), °C 1490
640
Melting Onset (Solidus), °C 1450
640
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 26
230
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 9.3
60
Electrical Conductivity: Equal Weight (Specific), % IACS 10
200

Otherwise Unclassified Properties

Base Metal Price, % relative 11
9.5
Density, g/cm3 7.9
2.7
Embodied Carbon, kg CO2/kg material 2.8
8.3
Embodied Energy, MJ/kg 40
160
Embodied Water, L/kg 89
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140
17 to 25
Resilience: Unit (Modulus of Resilience), kJ/m3 650
3.8 to 24
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 24
8.2 to 8.6
Strength to Weight: Bending, points 22
15 to 16
Thermal Diffusivity, mm2/s 6.9
93
Thermal Shock Resistance, points 19
3.6 to 3.7

Alloy Composition

Aluminum (Al), % 0 to 0.020
99.35 to 100
Boron (B), % 0.0010 to 0.0060
0
Carbon (C), % 0.070 to 0.13
0
Chromium (Cr), % 8.5 to 9.5
0
Copper (Cu), % 0
0 to 0.050
Iron (Fe), % 85.8 to 89.1
0 to 0.65
Magnesium (Mg), % 0
0 to 0.050
Manganese (Mn), % 0.3 to 0.6
0 to 0.050
Molybdenum (Mo), % 0.3 to 0.6
0
Nickel (Ni), % 0 to 0.4
0
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 0.65
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0 to 0.010
0 to 0.060
Tungsten (W), % 1.5 to 2.0
0
Vanadium (V), % 0.15 to 0.25
0 to 0.050
Zinc (Zn), % 0
0 to 0.1
Zirconium (Zr), % 0 to 0.010
0