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7049 Aluminum vs. SAE-AISI 4340M Steel

7049 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 (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 7049 aluminum and the bottom bar is SAE-AISI 4340M steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 140
710
Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 6.2 to 7.0
6.0
Fatigue Strength, MPa 160 to 170
690
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 27
72
Shear Strength, MPa 300 to 310
1360
Tensile Strength: Ultimate (UTS), MPa 510 to 530
2340
Tensile Strength: Yield (Proof), MPa 420 to 450
1240

Thermal Properties

Latent Heat of Fusion, J/g 370
280
Maximum Temperature: Mechanical, °C 180
430
Melting Completion (Liquidus), °C 640
1440
Melting Onset (Solidus), °C 480
1400
Specific Heat Capacity, J/kg-K 860
480
Thermal Conductivity, W/m-K 130
38
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 36
7.8
Electrical Conductivity: Equal Weight (Specific), % IACS 110
9.1

Otherwise Unclassified Properties

Base Metal Price, % relative 10
3.9
Density, g/cm3 3.1
7.8
Embodied Carbon, kg CO2/kg material 8.1
1.9
Embodied Energy, MJ/kg 140
26
Embodied Water, L/kg 1110
55

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 31 to 34
120
Resilience: Unit (Modulus of Resilience), kJ/m3 1270 to 1440
4120
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 46 to 47
84
Strength to Weight: Bending, points 46 to 47
51
Thermal Diffusivity, mm2/s 51
10
Thermal Shock Resistance, points 22 to 23
70

Alloy Composition


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Aluminum (Al), % 85.7 to 89.5
0
Carbon (C), % 0
0.38 to 0.43
Chromium (Cr), % 0.1 to 0.22
0.7 to 1.0
Copper (Cu), % 1.2 to 1.9
0
Iron (Fe), % 0 to 0.35
93.3 to 94.8
Magnesium (Mg), % 2.0 to 2.9
0
Manganese (Mn), % 0 to 0.2
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 to 0.25
1.5 to 1.8
Sulfur (S), % 0
0 to 0.012
Titanium (Ti), % 0 to 0.1
0
Vanadium (V), % 0
0.050 to 0.1
Zinc (Zn), % 7.2 to 8.2
0
Residuals, % 0 to 0.15
0