Aerospace Materials: CH2 AISI 4130 SHEET STRIP PLATE BARS and FORGINGS NORMALIZED and TEMPERED STRESS RELIEVEDA 0 188 B 2 3 1 0 G1 C1
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) | Fbru ksi 2 (ksi) | Fbry ksi 2 (ksi) | Fcy ksi (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Fty ksi (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | designation | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 AISI 4130 SHEET STRIP PLATE BARS AND FORGINGS NORMALIZED AND TEMPERED STRESS RELIEVEDA 0 188 B 2 3 1 0 G1 C1 | 70 | 29 | 29 | 200 | 129 | 75 | 57 | 95 | 75 | 11 | b | Normalized and tempered, stress relieveda | 0.283 | AISI 4130 | Sheet, strip, plate, bars, and forgings | 0.32 | AMS 6350 | <=0.188 |
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