Materials / Compare
Aluminum 6061-T6 vs. Nickel Inconel 718
Compare Aluminum 6061-T6 vs. Nickel Inconel 718 strength, stiffness, weight and thermal properties.
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|---|---|---|
| Mechanical | ||
| Yield strength | 276MPasourcetypical, 0.2% offset, .500 in dia specimen | 1,207MPasourcetypical, 1.0 in. hot-rolled bar, 0.2% offset |
| Ultimate tensile strength | 310MPasourcetypical | 1,389MPasourcetypical, 1.0 in. bar |
| Elongation at break | 17%sourcetypical, in 4D, 0.500 in dia specimen | 20%sourcetypical, 1.0 in. bar |
| Young's modulus (stiffness) | 68.3GPasourcetypical | 200GPasourcetypical, 21 °C, annealed + aged |
| Density | 2,700kg/m³sourcenominal | 8,221kg/m³sourcenominal, annealed and aged |
| Strength to weight | 102kN·m/kg | 147kN·m/kg44% higher |
| Stiffness to weight | 25.3MN·m/kg4% higher | 24.3MN·m/kg |
| Poisson's ratio | 0.33sourcetypical (handbook physical constant) | 0.294sourcetypical, 21 °C, annealed + aged |
| Shear modulus | 25.7GPa | 77.3GPa3.01x stiffer in shear |
| Bulk modulus | 67GPa | 162GPa |
| Speed of sound | 5,030m/s | 4,932m/s |
| Thermal | ||
| Thermal conductivity | 167W/m·Ksourcetypical, 20 °C | 11.4W/m·Ksourcetypical, 21 °C, annealed + aged (calculated from resistivity per footnote a) |
| Thermal expansion | 23.6µm/m·Ksourcetypical, mean 20-100 °C | 13.2µm/m·Ksourcetypical, mean 21-93 °C, annealed + aged |
| 100 mm part over a 50 °C swing | 118µm growth | 66µm growth1.79x less |
| Specific heat | 896J/kg·Ksourcetypical, at 100 °C | 435J/kg·Ksourcetypical, 21 °C |
| Heats up and cools (diffusivity) | 69mm²/s21.7x faster | 3.19mm²/s |
| Thermal shock resistance | 19,159W/m5.21x more resistant | 3,680W/m |
| Melting point | 582–652°Csourcesolidus-liquidus | 1,260–1,336°Csourcemelting range |
| Max service temperature | not sourced | 704°Csourceupper use temperature stated by producer |
| Values for | 6061-T6/T651, Kaiser Aluminum typical properties; Poisson from MIL-HDBK-5J | INCONEL alloy 718, standard grade, 1750 °F/1 hr anneal + 1325 °F/8 hr F.C. to 1150 °F aged; Special Metals bulletin SMC-045 typical values |
Every value links to the document that states it. "Not sourced" means no citable source states it (or only a specification minimum); figures computed from it are left out too.
Questions
Is Aluminum 6061-T6 stronger than Nickel Inconel 718?
Nickel Inconel 718 is stronger: its yield strength is 1,207 MPa against 276 MPa for Aluminum 6061-T6 (4.37x).
Which is lighter, Aluminum 6061-T6 or Nickel Inconel 718?
Aluminum 6061-T6 is lighter: 2,700 kg/m³ against 8,221 kg/m³ for Nickel Inconel 718.
Which is stiffer, Aluminum 6061-T6 or Nickel Inconel 718?
Nickel Inconel 718 is stiffer: Young's modulus 200 GPa against 68.3 GPa for Aluminum 6061-T6, so the same part in Nickel Inconel 718 deflects less under the same load.
Which is lighter for the same job, Aluminum 6061-T6 or Nickel Inconel 718?
For the same stiffness or strength: Aluminum 6061-T6 is lighter for a stiff rod or tie (tension), stiff beam (bending), stiff panel or plate, strong beam, strong panel or plate; Nickel Inconel 718 is lighter for a strong rod or tie.
| Part that must be | Aluminum 6061-T6 | Nickel Inconel 718 |
|---|---|---|
| Stiff rod or tie (tension) | lighter | 4% heavier |
| Stiff beam (bending) | lighter | 1.78x heavier |
| Stiff panel or plate | lighter | 2.13x heavier |
| Strong rod or tie | 44% heavier | lighter |
| Strong beam | lighter | 14% heavier |
| Strong panel or plate | lighter | 46% heavier |
For the same stiffness or strength, mass scales with density over stiffness (or strength) raised to a power set by how the part is loaded: 1 for a rod in tension, 1/2 for a beam in bending, 1/3 for a panel (the standard material-selection indices).
Which conducts heat better, Aluminum 6061-T6 or Nickel Inconel 718?
Aluminum 6061-T6 conducts heat better: 167 W/m·K against 11.4 W/m·K for Nickel Inconel 718.
Which expands less with temperature?
Nickel Inconel 718 expands less: 13.2 µm/m·K against 23.6 µm/m·K for Aluminum 6061-T6.
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