Fig. 8 Stress at fracture versus strain rate in slow-strain-rate SCC tests of AZ91. The specimens were partially immersed in distilled water. Strain was controlled with a linear ramp to maintain the desired strain rate. Source: Ref 11 More

Fig. 4.7 Effect of stress intensity on the growth rate of stress corrosion cracks in type 304L stainless steel exposed to magnesium chloride and sodium chloride solutions. After Ref 4.27 More

Fig. 13 Effect of stress intensity on the growth rate of stress-corrosion cracks in type 304L stainless steel exposed to magnesium chloride and sodium chloride solutions More

Fig. 7.103 Typical subcritical stress-corrosion crack propagation rate versus stress intensity. Source: Ref 115 More

Fig. 7.104 Effect of stress intensity on stress-corrosion crack growth rate for type 304L stainless steel in aerated MgCl 2 at 130 °C. Symbols indicate whether propagation occurs as a single or branched crack. Source: Ref 165 More

Fig. 7.109 Effect of stress intensity on the growth rate of stress-corrosion cracks in several austenitic stainless steels. Alloy compositions can be found in Ref 166 . Redrawn from Ref 166 More

Fig. 7.113 Dependence of stress-corrosion-crack-growth rate on stress intensity of a high-strength aluminum alloy in several aqueous environments. Crack orientation TL (stress in transverse direction; crack propagation in longitudinal direction). Source: Ref 159 More

Fig. 7.114 Dependence of stress-corrosion-crack-growth rate on stress intensity for a high-strength aluminum alloy at various temperatures. Source: Ref 159 More

Fig. 7.115 Dependence of stress-corrosion-crack-growth rate on stress intensity for a high-strength aluminum alloy at several relative humidities. Crack orientation TL (stress in transverse direction, crack propagation in longitudinal direction). Source: Ref 159 More

Fig. 12.21 Effect of cooling rate on stress-rupture life of a cast nickel-base superalloy at 982 °C (1800 °F)/200 MPa (29 ksi) More

Figure 7.11 Sensitivity of flow stress to strain rate change as a function of temperature for pure copper and pure iron ( Basinski, 1959 ; Basinski and Christian, 1960 ). More

Fig. 20.6 Effect of deformation rate and temperature on flow stress of Ti-6Al-6V-2Sn alloy under isothermal forging conditions [ Fix, 1972 ] More

Fig. 13 Flow stress vs. strain rate for 6063-O aluminum. Source: Ref 7 More

Fig. 5.14 Effect of strain rate on flow stress ( t 0 = 1 mm; T = 200 °C, or 390 °F). Source: Ref 5.6 More

Fig. 12 Effect of stress relieving on corrosion rate of type 347 stainless steel in boiling 65% HNO 3 . All stress-relief treatments lasted 2 hours. More

Fig. 2.54 Schematic influence of strain rate on yield stress. Source: Ref 2.6 More

Fig. 2.86 Variation of minimum creep rate with stress for a nomalized-and-tempered 1.25Cr-0.5Mo steel. The letters T and I denote transgranular and intergranular failure, respectively. Source: Ref 2.50 More

Fig. 3.9 Effect of cooling rate on magnesium casting tensile stress-strain curves. Schematic; not drawn to scale. Source: Ref 3.2 More

Fig. 5.51 Effect of stress ratio on fatigue crack growth rate threshold for several aluminum alloys. Source: Ref 5.27 More

Fig. 5.52 Effect of stress ratio on fatigue crack growth rate threshold for titanium alloys. Source: Ref 5.54 More