Sample data from Engineering Database — 375 reference tables, deterministic calculators, and Engineering AI. Sign up free

Aerospace Materials: 7055 EXTRUSION T76511

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: 7055 EXTRUSION T765114 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)basisconditiondensity lb in3 (lb/in^3)elongation pct (%)formpoisson ratiospecificationthickness range
7055 EXTRUSION T76511 0.250-0.499 A7010.410.8124161105124858647908485793.9AT765110.1039Extrusion0.33AMS 43360.250-0.499
7055 EXTRUSION T76511 0.250-0.499 B7010.410.8129169112132919249948791853.9BT765110.103Extrusion0.33AMS 43360.250-0.499
7055 EXTRUSION T76511 LE0.249 A7010.410.8122160105124848646898385793.9AT765110.1037Extrusion0.33AMS 4336<=0.249
7055 EXTRUSION T76511 LE0.249 B7010.410.8125163107127868847918587813.9BT765110.103Extrusion0.33AMS 4336<=0.249

What else is in Engineering Database

Related data