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Aerospace Materials: TI-6AL-4V SHEET UNK

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 SHEET UNK10 rows
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)Fcy ksi LT (ksi)Fsu ksi (ksi)Ftu ksi (ksi)Ftu ksi LT (ksi)Fty ksi (ksi)Fty ksi LT (ksi)G Msi (Msi)basisdensity lb in3 (lb/in^3)elongation pct (%)elongation pct LT (%)formpoisson ratio
TI-6AL-4V SHEET UNK ANY A T5 4 1 0b C1701616.4213272171208133135871341341261266.2A0.1688Sheet, strip, and plate0.31
TI-6AL-4V SHEET UNK ANY A T5 4 1 0b C3701616.4206260164194124130791301301201206.2A0.161010Sheet, strip, and plate0.31
TI-6AL-4V SHEET UNK ANY A T5 4 1 0b C5701616.4206260161191122128791301301181186.2A0.161010Sheet, strip, and plate0.31
TI-6AL-4V SHEET UNK ANY B T5 4 1 0b C2701616.4221283178217138141901391391311316.2B0.16Sheet, strip, and plate0.31
TI-6AL-4V SHEET UNK ANY B T5 4 1 0b C4701616.4214276179212129142841351381251316.2B0.16Sheet, strip, and plate0.31
TI-6AL-4V SHEET UNK ANY B T5 4 1 0b C6701616.4217274176209127140841371371231296.2B0.16Sheet, strip, and plate0.31
TI-6AL-4V SHEET UNK ANY S T5 4 1 0b C10701616.41451451351356.2S0.1666Sheet, strip, and plate0.31
TI-6AL-4V SHEET UNK ANY S T5 4 1 0b C7701616.42362862102321541621001601601451456.2S0.1655Sheet, strip, and plate0.31
TI-6AL-4V SHEET UNK ANY S T5 4 1 0b C8701616.4248308210243150931601601451456.2S0.1688Sheet, strip, and plate0.31
TI-6AL-4V SHEET UNK ANY S T5 4 1 0b C9701616.4233289203235145871501501401406.2S0.1666Sheet, strip, and plate0.31

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