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Aerospace Materials: TI-6AL-4V BAR CROSS-SECTIO

Aerospace material mechanical properties and design allowables at ambient, elevated, and cryogenic temperatures per MMPDS-11 (Metallic Materials Properties Development and Standardization). Covers primary structural alloys: aluminum (2024-T3, 7075-T6, 6061-T6, 2219-T87), titanium (Ti-6Al-4V), nickel superalloys (Inconel 718), and steels (300M, 4130, 4340).

Materials Sciencematerial id: TI-6AL-4V BAR CROSS-SECTIO3 rowsPage 2 of 2
material idtemp fE Msi (Msi)Ec Msi (Msi)Fbru ksi (ksi)Fbru ksi 2 (ksi)Fbry ksi (ksi)Fbry ksi 2 (ksi)Fcy ksi (ksi)Fsu ksi (ksi)Ftu ksi (ksi)Ftu ksi LT (ksi)Fty ksi (ksi)Fty ksi LT (ksi)G Msi (Msi)RA pct (%)RA pct LT (%)basisconditiondensity lb in3 (lb/in^3)elongation pct (%)elongation pct LT (%)formpoisson ratio
TI-6AL-4V BAR CROSS-SECTIO ANY B T5 4 1 0c2 C77016.917.21381421281316.5BCross-sectional area, in.20.16Bar0.31
TI-6AL-4V BAR CROSS-SECTIO ANY B T5 4 1 0c2 C97016.917.21351411251296.5BCross-sectional area, in.20.16Bar0.31
TI-6AL-4V BAR CROSS-SECTIO ANY S7016.917.2194244170197124801301301201206.52525SCross-sectional area, in.20.161010Bar0.31

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