Fig. 8.33 Effect of impact energy on damage size. Source: Ref 8.40 More

Fig. 8.34 Effect of impact energy on dent depth. Source: Ref 8.40 More

Fig. 18.10 Impact energy cutoff diagram. Source: Ref 4 More

Fig. 10.4 Dependence of notched impact energy on tempering temperature for 0.4 and 0.5% C steels. TME, tempered martensite embrittlement. Source: Ref 10.2 More

Fig. 19 Influence of phosphorus and antimony on room-temperature impact energy as a function of tempering temperature in a Ni-Cr-Mo steel. Arrow shows the laboratory alloy. Source: Ref 19 More

Fig. 15.38 Impact energy absorbed as a function of isothermal transformation temperature for specimens of 4340 steel. E 0 , total energy absorbed; E 1 , fracture initiation energy; E 2 , fracture propagation energy. Source: Ref 15.24 as published in Ref 15.19 More

Fig. 6.14 Impact energy absorbed as a function of isothermal transformation temperature for specimens of 4340 steel. E 0 is total energy absorbed, E 1 is fracture initiation energy, and E 2 is fracture propagation energy. Source: Ref 6.16 More

Fig. 8.7 Variation in Charpy V-notch impact energy with temperature for normalized plain carbon steels of varying carbon content More

Fig. 8.8 Variation in Charpy V-notch impact energy with microstructure and carbon content for 0.70Cr-0.32Mo steel. Carbon content levels: (a) 0.17% and (b) 0.40%. A pearlitic structure was formed by transformation at 650 °C (1200 °F). A structure with 50% martensite was formed by quenching More

Fig. 17.10 Variation in Charpy V-notch impact energy with temperature for furnace-cooled Fe-Mn-0.05C alloys containing varying amounts of manganese More

Fig. 17.11 Variation in Charpy V-notch impact energy with temperature for low-carbon steels containing varying amounts of niobium that were normalized from 955 °C (1750 °F) More

Fig. 31 Impact energy cut-off diagram. Source: Ref 17 More

Fig. 1.26 Variations of (a) unnotched impact energy and (b) bending strength (15 × 60 × 2 mm). A: vacuum-carburized, 1040 °C, reheat quenched. B: vacuum-carburized, 1040 °C, direct quenched. C: vacuum carburized, 930 °C, reheat quenched. D3: gas-carburized, 920 °C, direct quenched. Source More

Fig. 12.3 Effects of hydrogen content and heat treatment on the impact energy of alpha titanium More

Fig. 12.4 Effects of hydrogen content and heat treatment on the impact energy of commercial purity titanium More

Fig. 7-16 Torsion impact energy absorbed as a function of tempering temperature for 1% C tool steel austenitized at various temperatures as shown. Source: Ref 19 More

Fig. 8-16 Torsional impact energy absorbed as a function of tempering temperature for high-carbon L-type steels. Curve 1, Bethlehem Steel Co.; curves 2 and 3, Ref 21 Curve Composition, % Hardening temperature Hardening medium C Cr V °C °F 1 0.70 0.80 0.20 800 1475 More

Fig. 8-25 Notched Izod impact energy absorbed versus tempered hardness for medium-carbon L2 steels. Curve 1, Ref 25 ; curve 2, Allegheny Ludlum Industries; curve 3, Teledyne VASCO Curve Composition, % Hardening temperature Hardening medium C Mn Cr Mo V °C °F 1 0.50 More

Fig. 8-32 Effect of tempering temperature on impact energy absorbed by L6-type steels. Curve 1, torsion impact, Ref 27 ; curve 2, unnotched Izod impact test, Allegheny Ludlum Industries; curve 3, unnotched, Bethlehem Steel Co. Curve Composition, % Hardening temperature Hardening More

Fig. 9-10 Impact energy absorbed as a function of tempering temperature during unnotched Charpy and torsion impact testing of S1 steel specimens. Data from Bethlehem Steel Co. Curve Test Composition, % Quenching temperature Quenching medium C Si W Cr V °C °F 1 More