Aerospace Materials: MG-AZ31B EXTRUSION TUBE F
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).
| material id | temp f | E Msi (Msi) | Ec Msi (Msi) | Fcy ksi (ksi) | Ftu ksi (ksi) | Fty ksi (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| MG-AZ31B EXTRUSION TUBE F 0.028-0.250 S | 70 | 6.5 | 6.5 | 10 | 32 | 16 | 2.4 | S | F | 0.0639 | 8 | Extruded tube | 0.35 | ASTM B 107 | 0.028-0.250a |
| MG-AZ31B EXTRUSION TUBE F 0.251-0.750 S | 70 | 6.5 | 6.5 | 10 | 32 | 16 | 2.4 | S | F | 0.0639 | 4 | Extruded tube | 0.35 | ASTM B 107 | 0.251-0.750a |
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