Fig. 9.16 Geometry of notched-bar impact test specimens. Simple beam Charpy specimens: (a) V-notch, (b) keyhole-notch, and (c) cantilever beam notched Izod. Source: Ref 1 More

Fig. 28 Test fixtures for the K Ic test specimens. (a) Fixtures for the bend test. (b) Clevises for the compact specimen. Source: Ref 12 More

Fig. 8.3 Test specimens and test techniques for filament-wound composites. Source: Ref 8.16 More

Fig. 6 Schematic of (a) corrosion test specimens and (b) crevice corrosion test results for cold-rolled steel (CRS), 60 g/m 2 electrogalvanized steel (EG60), and three aluminum alloys (2036, 5182, and 6111). The crevice corrosion is measured in terms of the maximum depth of pitting attack More

Fig. 4.16 Example test specimens from bulge test More

Fig. 11 Three Charpy V-notch impact test specimens of the same metallurgical conditions tested at three different temperatures. At the highest temperature (left), the fracture is virtually all shear. At intermediate temperature (center), the fracture is combined shear and cleavage More

Fig. 13.19 Fracture toughness test specimens. Source: Ref 9 More

Fig. 9.7 Test specimens alloy HR-160, 625, 800H, RA330, and Type 310 at 900 °C (1650 °F) in the combustion gas stream generated by a burner rig using No. 2 fuel oil (0.4% S) for combustion at 35:1 air-to-fuel ratio and with injection of 50 ppm sea salt into the combustion gas stream. During More

Fig. 24-75 (a) Relation between the fraction of the test specimens that quench cracked and M s temperature. (b) Relation between fraction of the test specimens that quench cracked and Ceq ( 60 ) More

Fig. 9 Specifications for cruciform cracking test specimens. Source: Ref 3 More

Fig. 10 Sample specifications for implant test specimens. Source: Ref 3 More

Fig. 19 Fatigue limits of plasma- and gas-carburized test specimens as a function of retained austenite content More

Fig. 38 The case and core microstructure of carburized SAE 8620 test specimens (0.95% C potential); carburized at 955 °C (1750 °F), quenched into a 50:50 mixture of sodium nitrate and potassium nitrate at 250 °C (480 °F), held 120 min, then air cooled and tempered at 250 °C (480 °F) for 240 More

Fig. 17.18 Typical tuning fork SCC test specimens. (a) Source: Ref 17.19 . (b) Source: Ref 17.4 . (c) Source: Ref 17.21 More

Fig. 17.22 Stress-corrosion cracking test specimens containing residual stresses from plastic deformation. (a) Cracked cup specimen (Ericksen impression). Source: Ref 17.4 . (b) Joggled extrusion containing SCC in the plastically deformed region. Source: Ref 17.9 More

Fig. 17.23 Stress-corrosion cracking test specimens containing residual stresses from plastic deformation. Shown are 12.7 mm (0.5 in.) diameter stainless tubular specimens after SCC testing. (a) and (b) Annealed tubing that was cold formed before testing. (c) Cold worked tubing tested More

Fig. 17 Three Charpy V-notch impact test specimens of the same metallurgical conditions tested at three different temperatures. At the highest temperature (left), the fracture is virtually all shear. At intermediate temperature (center), the fracture is combined shear and cleavage More

Fig. 9.27 Typical analog test specimens for characterization and aging. JANNAF: Joint Army, Navy, NASA, Air Force More

Fig. 5.1 Test specimens for ring versus cylinder wear testing More