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Aerospace Materials: CLAD 2014 PLATE T651

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 2014 PLATE T6518 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)Fcy ksi ST (ksi)Fsu ksi (ksi)Ftu ksi (ksi)Ftu ksi LT (ksi)Ftu ksi ST (ksi)Fty ksi (ksi)Fty ksi LT (ksi)Fty ksi ST (ksi)G Msi (Msi)basisconditionelongation pct LT (%)formpoisson ratiospecificationthickness range
CLAD 2014 PLATE T651 1.001-2.000 A7010.710.910112885100555838636457564AT651a4Plate0.33AMS-QQ-A-250/31.001-2.000b
CLAD 2014 PLATE T651 1.001-2.000 B7010.710.910213088104576038646559584BT651aPlate0.33AMS-QQ-A-250/31.001-2.000b
CLAD 2014 PLATE T651 2.001-2.500 A7010.710.9971248498545759376162595655544AT651a2Plate0.33AMS-QQ-A-250/32.001-2.500b
CLAD 2014 PLATE T651 2.001-2.500 B7010.710.99912687102565961376263605857564BT651aPlate0.33AMS-QQ-A-250/32.001-2.500b
CLAD 2014 PLATE T651 2.501-3.000 A7010.710.960544AT651a2Plate0.33AMS-QQ-A-250/32.501-3.000b
CLAD 2014 PLATE T651 2.501-3.000 B7010.710.961564BT651aPlate0.33AMS-QQ-A-250/32.501-3.000b
CLAD 2014 PLATE T651 3.001-4.000 A7010.710.956524AT651a1Plate0.33AMS-QQ-A-250/33.001-4.000b
CLAD 2014 PLATE T651 3.001-4.000 B7010.710.957544BT651aPlate0.33AMS-QQ-A-250/33.001-4.000b

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