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. 1.28 Crack growth rate vs. elastic-plastic stress intensity for iron and nickel tested in 1 N H 2 SO 4 at given cathodic overpotentials (COP). (a) 2 mm (0.08 in.) thick iron and nickel. (b) 10 mm (0.4 in.) thick iron and nickel More

Fig. 1.29 Typical subcritical crack propagation rate vs. stress-intensity relationship. Stress intensity, K , is defined as K = A σ π C / B , where σ is the total tensile stress, C is the crack length, and A and B are geometrical constants. More

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

Fig. 3.25 Crack growth rate as a function of stress intensity in steels B6 and B7 compared with that of steel B2. Source: Ref 3.40 More

Fig. 3.42 Effects of temperature and stress intensity on crack growth rate in water and water-saturated argon environments. Source: Ref 3.49 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. 12.13 Flow stress versus strain rate for 6063-O aluminum. Source: Ref 6 More

Fig. 1 Stress-strain behavior of polycarbonate as a function of strain rate, λ ˙ , at 22.2 °C (72 °F). (Note: For small strains, extension, e , is approximately equal to engineering strain, ε.) More

Fig. 2 Strain-rate and temperature dependence of yield stress for polycarbonate More

Fig. 3 Stress-strain behavior of polyether-imide as a function of strain rate, λ ˙ , at 22.2 °C (72 °F). (Note: For small strains, extension, e , is approximately equal to engineering strain, ε.) More