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

Aerospace Materials: CLAD 2524 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: CLAD 2524 SHEET UNK7 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)basiselongation pct LT (%)formpoisson ratiospecificationthickness range
CLAD 2524 SHEET UNK 0.032- S709.81093117657638424059594439S15Sheet and Plate0.35AMS 42960.032-
CLAD 2524 SHEET UNK 0.063-0.128 A709.81097121677839434161614540A15Sheet and Plate0.35AMS 42960.063-0.128
CLAD 2524 SHEET UNK 0.063-0.128 B709.81098123708241454262624742BSheet and Plate0.35AMS 42960.063-0.128
CLAD 2524 SHEET UNK 0.129-0.249 A709.81098123677839434262624540A15Sheet and Plate0.35AMS 42960.129-0.249
CLAD 2524 SHEET UNK 0.129-0.249 B709.81098123698040444262624641BSheet and Plate0.35AMS 42960.129-0.249
CLAD 2524 SHEET UNK 0.250-0.310 A709.81098123677839434262624540A15Sheet and Plate0.35AMS 42960.250-0.310
CLAD 2524 SHEET UNK 0.250-0.310 B709.810100125698040444363634641BSheet and Plate0.35AMS 42960.250-0.310

What else is in Engineering Database

Related data