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ASTM A182 Grade F3V vs. 356.0 Aluminum

ASTM A182 grade F3V belongs to the iron alloys classification, while 356.0 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 F3V and the bottom bar is 356.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 210
55 to 75
Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 20
2.0 to 3.8
Fatigue Strength, MPa 330
55 to 75
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 74
27
Shear Strength, MPa 410
140 to 190
Tensile Strength: Ultimate (UTS), MPa 660
160 to 240
Tensile Strength: Yield (Proof), MPa 470
100 to 190

Thermal Properties

Latent Heat of Fusion, J/g 250
500
Maximum Temperature: Mechanical, °C 470
170
Melting Completion (Liquidus), °C 1470
620
Melting Onset (Solidus), °C 1430
570
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 39
150 to 170
Thermal Expansion, µm/m-K 13
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.6
40 to 43
Electrical Conductivity: Equal Weight (Specific), % IACS 8.8
140 to 150

Otherwise Unclassified Properties

Base Metal Price, % relative 4.2
9.5
Density, g/cm3 7.9
2.6
Embodied Carbon, kg CO2/kg material 2.3
8.0
Embodied Energy, MJ/kg 33
150
Embodied Water, L/kg 63
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
3.2 to 8.2
Resilience: Unit (Modulus of Resilience), kJ/m3 590
70 to 250
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 24
53
Strength to Weight: Axial, points 23
17 to 26
Strength to Weight: Bending, points 21
25 to 33
Thermal Diffusivity, mm2/s 10
64 to 71
Thermal Shock Resistance, points 19
7.6 to 11

Alloy Composition

Aluminum (Al), % 0
90.1 to 93.3
Boron (B), % 0.0010 to 0.0030
0
Carbon (C), % 0.050 to 0.18
0
Chromium (Cr), % 2.8 to 3.2
0
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 94.4 to 95.7
0 to 0.6
Magnesium (Mg), % 0
0.2 to 0.45
Manganese (Mn), % 0.3 to 0.6
0 to 0.35
Molybdenum (Mo), % 0.9 to 1.1
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.1
6.5 to 7.5
Sulfur (S), % 0 to 0.020
0
Titanium (Ti), % 0.015 to 0.035
0 to 0.25
Vanadium (V), % 0.2 to 0.3
0
Zinc (Zn), % 0
0 to 0.35
Residuals, % 0
0 to 0.15