Fig. 4.32 Effect of temperature and strain rate on plane-strain fracture toughness behavior of ASTM type A36 steel. Source: Ref 4.36 More

Fig. 1 Plane-strain fracture toughness of maraging steels compared with fracture toughness of several ultrahigh strength steels as a function of tensile strength. More

Fig. 11 Specimen types used in plane-strain fracture-toughness ( K Ic ) testing (ASTMA 399). a , crack length; W , specimen width More

Fig. 32 Relation between plane-strain fracture toughness ( K Ic ) and Charpy V-notch (CVN) impact energy. Tests conducted at 27 °C (80 °F). VM, vacuum melted; AM, air melted. Source: Ref 3 More

Fig. 26 Relationships of plane-strain fracture toughness to yield strength for the 2 xxx and 7 xxx series of aluminum alloys. Source: Ref 12 More

Fig. 17.26 Plane-strain fracture toughness as a function of the ultimate tensile strength for vacuum hot pressed (VHP) S-65 and VHP S-200E. First and second letters refer to sample and crack orientation, respectively, relative to the VHP billet. L, longitudinal (parallel to the pressing More

Fig. 4.14 MIL-HDBK-5 B-scale plane-strain fracture toughness values for D6AC steel as a function of heat treatment. Heat treatment designations refer to Table 4.5 . Source: Ref 4.21 More

Fig. 4.15 Effects of alloying element content on plane-strain fracture toughness of high-strength steel (Fe-0.65Mn-0.35Si-0.8Cr-0.3Mo-0.1V). (a) Holding carbon at 0.35% and varying the amount of nickel. (b) Holding nickel at 3% and varying the amount of carbon. All steels were hardened More

Fig. 4.38 Relation ( Eq 4.13b ) between plane-strain fracture toughness and CVN impact energy. Tests conducted at 27 °C (81 °F). VM, vacuum melted; AM, air melted. Source: Ref 4.36 , 4.40 More

Fig. 8.23 Plane-strain fracture toughness, K Ic , versus tensile yield strength for selected aluminum alloy castings. SC, sand cast alloy; PE, premium engineered alloy More

Fig. 8.24 Plane-strain fracture toughness, K Ic , versus notch-yield ratio for some cast aluminum alloys compared to the mean values of the relationship for wrought aluminum alloys More

Fig. 8.25 Plane-strain fracture toughness, K Ic , versus notch-yield ratio for selected cast aluminum alloys compared to the range of such values for wrought aluminum alloys. SC, sand cast; PM, permanent mold More

Fig. A3.7 Compact tension plane strain fracture toughness specimen. Refer to ASTM E 399. More

Fig. A7.2 Plane-strain fracture toughness as a function of material tensile yield strength. Comparison of several 2000 and 7000 series aluminum alloys. Source: Ref A7.1 More

Fig. A7.3 Plane-strain fracture toughness for 25.4 to 38.1 mm (1 to 1.5 in.) thick commercial aluminum alloys. Source: Ref A7.6 More

Fig. A8.1 Plane-strain fracture toughness as a function of material tensile yield strength for four-point notch-bend specimens of mill-annealed Ti-6Al-4V. Source: Ref A8.2 More

Fig. A10.2 Room-temperature plane-strain fracture toughness for several high-strength steels. Source: Ref A10.1 More

Fig. A10.3 Plane-strain fracture toughness of 4345 steel as function of tensile yield strength and sulfide content. Source: Ref A10.2 More

Fig. A10.4 Room-temperature plane-strain fracture toughness of 4340 steel as a function of tensile yield strength. Source: ○, Ref A10.3 ; ■, Ref A10.4 More

Fig. A10.5 Plane-strain fracture toughness of PH13-8Mo and Custom 465 precipitation-hardening stainless steels. ○, PH13-8Mo (Source: Ref A10.5 ); ●, PH13-8Mo (Source: Ref A10.1 ); ◊, Custom 465 (Source: Ref A10.1 ) More