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336.0 Aluminum vs. ASTM A369 Grade FP92

336.0 aluminum belongs to the aluminum alloys classification, while ASTM A369 grade FP92 belongs to the iron alloys. There are 31 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 336.0 aluminum and the bottom bar is ASTM A369 grade FP92.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 110 to 130
210
Elastic (Young's, Tensile) Modulus, GPa 75
190
Elongation at Break, % 0.5
19
Fatigue Strength, MPa 80 to 93
330
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 28
76
Shear Strength, MPa 190 to 250
440
Tensile Strength: Ultimate (UTS), MPa 250 to 320
710
Tensile Strength: Yield (Proof), MPa 190 to 300
490

Thermal Properties

Latent Heat of Fusion, J/g 570
260
Maximum Temperature: Mechanical, °C 210
590
Melting Completion (Liquidus), °C 570
1490
Melting Onset (Solidus), °C 540
1450
Specific Heat Capacity, J/kg-K 890
470
Thermal Conductivity, W/m-K 120
26
Thermal Expansion, µm/m-K 19
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
9.3
Electrical Conductivity: Equal Weight (Specific), % IACS 95
10

Otherwise Unclassified Properties

Base Metal Price, % relative 11
11
Density, g/cm3 2.8
7.9
Embodied Carbon, kg CO2/kg material 7.9
2.8
Embodied Energy, MJ/kg 140
40
Embodied Water, L/kg 1010
89

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.1 to 1.6
120
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 580
620
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 25 to 32
25
Strength to Weight: Bending, points 32 to 38
22
Thermal Diffusivity, mm2/s 48
6.9
Thermal Shock Resistance, points 12 to 16
19

Alloy Composition

Aluminum (Al), % 79.1 to 85.8
0 to 0.020
Boron (B), % 0
0.0010 to 0.0060
Carbon (C), % 0
0.070 to 0.13
Chromium (Cr), % 0
8.5 to 9.5
Copper (Cu), % 0.5 to 1.5
0
Iron (Fe), % 0 to 1.2
85.8 to 89.1
Magnesium (Mg), % 0.7 to 1.3
0
Manganese (Mn), % 0 to 0.35
0.3 to 0.6
Molybdenum (Mo), % 0
0.3 to 0.6
Nickel (Ni), % 2.0 to 3.0
0 to 0.4
Niobium (Nb), % 0
0.040 to 0.090
Nitrogen (N), % 0
0.030 to 0.070
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 11 to 13
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.25
0 to 0.010
Tungsten (W), % 0
1.5 to 2.0
Vanadium (V), % 0
0.15 to 0.25
Zinc (Zn), % 0 to 0.35
0
Zirconium (Zr), % 0
0 to 0.010