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. 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. 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. 1.34 Stress-corrosion crack growth as a function of the two strain-rate thresholds, ε ˙ 1 and ε ˙ 2 More

Fig. 7.21 Rate of stress-corrosion crack propagation as a function of σ g l in cold rolled brass exposed to 0.05 M CuSO 4 + 0.48 M (NH 4 ) 2 SO 4 (pH 7.25). Source: Ref 7.55 More

Fig. 17.38 Effects of beam deflection rate on stress-corrosion crack velocity in precracked cantilever bend specimens of a carbon-manganese steel. Tested in a carbonate-bicarbonate solution at 75 °C (165 °F) and at a potential of −650 mV (SCE). Source: Ref 17.58 More

Fig. 17.54 Stress-corrosion cracking propagation rates for various aluminum alloy 7050 products. Double-beam specimens (S-L; see Fig. 17.29 ) bolt-loaded to pop-in and wetted three times daily with 3.5% NaCl. Plateau velocity averaged over 15 days. The right-hand end of the band for each More

Fig. 7.112 Dependence of corrosion-crack-growth rate on stress intensity for two high-strength aluminum alloys in saturated NaCl solution at 23 °C. Crack orientation TL (stress in transverse direction; crack propagation in longitudinal direction). Source: Ref 159 More

Fig. 7.120 Corrosion-fatigue-crack-growth rate as a function of stress-intensity range for a maraging steel in air and 3% NaCl solution. Source: Ref 171 More

Fig. 7.121 Corrosion-fatigue-crack-growth rate as a function of stress-intensity range for high-strength 4340M steel in vacuum and distilled water at 23 °C. Data for vacuum and indicated frequencies and R = 0. Source: Ref 172 More

Fig. 7.122 Corrosion-fatigue-crack-growth rate as a function of stress-intensity range for X-65 line pipe steel in air and in 3.5% NaCl solution under cathodic coupling to zinc. Cycled at indicated frequencies and R = 0.2. Coupled potential = –800 ± 10 mV (SHE). (Note: Original reference More

Fig. 7.123 Corrosion-fatigue-crack-growth rate as a function of stress-intensity range for X-65 line pipe steel in air and at the free corrosion potential in 3.5% NaCl at indicated frequencies and R = 0.2. Corrosion potential = –440 ± 30 mV (SHE). (Note: Original reference includes data More

Fig. 7.124 Corrosion-fatigue-crack-growth rate as a function of stress-intensity range for Ti-6Al-4V alloy in air and in 0.6 M NaCl at indicated frequencies and R = 0.1. Source: Ref 170 More

Fig. 7.125 Corrosion-fatigue-crack-growth rate as a function of stress-intensity range for a high-strength aluminum alloy in dry argon and indicated halide solutions. Source: Ref 173 More

Fig. 17 Crack propagation rates in stress-corrosion tests using precracked specimens of high-strength 2 xxx series aluminum alloys, 25 mm thick, double antilever beam, T-L (S-L) orientation of plate, wet twice a day with an aqueous solution of 3.5% NaCl, 23 °C. Source: Ref 13 More