Aerospace Materials: CH2 AISI 8630 SHEET STRIP and PLATE NORMALIZED and TEMPERED STRESS RELIEVEDB 0 188 S 2 3 1 0 C1 C5
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 8630 SHEET STRIP AND PLATE NORMALIZED AND TEMPERED STRESS RELIEVEDB 0 188 S 2 3 1 0 C1 C5 | 70 | 29 | 29 | 200 | 129 | 75 | 57 | 95 | 75 | 11 | S | Normalized and tempered, stress relievedb | 0.283 | AISI 8630 | Sheet, strip, and plate | 0.32 | AMS-S-18728a | 0.188 |
What else is in Engineering Database
AI built for engineering. Searches the engineering database, performs calculations, gives source-backed engineering insights.
Get started for free ↗Reference Data375 engineering tablesMaterial properties, pipe and shape dimensions, code tables, and electrical ratings across mechanical, civil, chemical, electrical, materials, and manufacturing engineering.
Browse dataCalculatorsDeterministic engineering calculatorsSizing, checking, and conversion tools that run against the reference tables. Inputs are code-compliant, outputs are traceable to the source standard.
Browse calculators