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295.0 Aluminum vs. SAE-AISI 4340M Steel

295.0 aluminum belongs to the aluminum alloys classification, while SAE-AISI 4340M steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (5, 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 295.0 aluminum and the bottom bar is SAE-AISI 4340M steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 60 to 93
710
Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 2.0 to 7.2
6.0
Fatigue Strength, MPa 44 to 55
690
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
72
Shear Strength, MPa 180 to 230
1360
Tensile Strength: Ultimate (UTS), MPa 230 to 280
2340
Tensile Strength: Yield (Proof), MPa 100 to 220
1240

Thermal Properties

Latent Heat of Fusion, J/g 400
280
Maximum Temperature: Mechanical, °C 170
430
Melting Completion (Liquidus), °C 640
1440
Melting Onset (Solidus), °C 530
1400
Specific Heat Capacity, J/kg-K 880
480
Thermal Conductivity, W/m-K 140
38
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
7.8
Electrical Conductivity: Equal Weight (Specific), % IACS 100
9.1

Otherwise Unclassified Properties

Base Metal Price, % relative 10
3.9
Density, g/cm3 3.0
7.8
Embodied Carbon, kg CO2/kg material 7.9
1.9
Embodied Energy, MJ/kg 150
26
Embodied Water, L/kg 1140
55

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.2 to 13
120
Resilience: Unit (Modulus of Resilience), kJ/m3 77 to 340
4120
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 46
25
Strength to Weight: Axial, points 21 to 26
84
Strength to Weight: Bending, points 27 to 32
51
Thermal Diffusivity, mm2/s 54
10
Thermal Shock Resistance, points 9.8 to 12
70

Alloy Composition

Aluminum (Al), % 91.4 to 95.3
0
Carbon (C), % 0
0.38 to 0.43
Chromium (Cr), % 0
0.7 to 1.0
Copper (Cu), % 4.0 to 5.0
0
Iron (Fe), % 0 to 1.0
93.3 to 94.8
Magnesium (Mg), % 0 to 0.030
0
Manganese (Mn), % 0 to 0.35
0.65 to 0.9
Molybdenum (Mo), % 0
0.35 to 0.45
Nickel (Ni), % 0
1.7 to 2.0
Phosphorus (P), % 0
0 to 0.012
Silicon (Si), % 0.7 to 1.5
1.5 to 1.8
Sulfur (S), % 0
0 to 0.012
Titanium (Ti), % 0 to 0.25
0
Vanadium (V), % 0
0.050 to 0.1
Zinc (Zn), % 0 to 0.35
0
Residuals, % 0 to 0.15
0