Search Results for Stress-intensity

Fig. 18.18 Concept of threshold stress intensity ( K Iscc ). K Ic , fracture stress intensity 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. 14 Effect of nickel content on the stress-corrosion threshold stress intensity of various alloys in an aerated aqueous 22% NaCl solution at 105 °C (220 °F). Alloys X and Y are German heat-resistant grades. 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. 4.8 Effect of nickel content on the stress-corrosion threshold stress intensity of various alloys in an aerated aqueous 22% NaCl solution at 105 °C (220 °F). Alloys X and Y are German heat-resistant grades. After Ref 4.27 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. 7.110 Effect of nickel content on stress-corrosion threshold stress intensity of Fe-Ni-Cr alloys with about 18% Cr. Alloy compositions can be found in Ref 166 . 2H = AISI 431, untempered martensite. 4S = AISI 431, sensitized. Source: Ref 166 More

Fig. 7.111 Effect of molybdenum content on stress-corrosion threshold stress intensity of austenitic stainless steels. Source: 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. 14 The effect of electrode potential and stress intensity on stress corrosion crack velocity in a high strength aluminum alloy (7079-T651). 2.5 cm thick plate. T-L crack orientation (long transverse grain direction normal to the fracture plane; longitudinal direction of crack propagation More

Fig. 15 Effect of temperature and stress intensity on the stress-corrosion crack velocity in high-strength aluminum alloy (7039-T61) exposed to distilled water. 2.5 cm thick plate. S-L crack orientation (short transverse grain direction normal to the fracture plane; longitudinal direction More

Fig. 4.20 Stress corrosion cracking velocity versus stress intensity factor. (a) Type A, dotted line; type B, solid line. (b) Type C behavior More

Fig. 5.34 Center-cracked panel stress-intensity solutions based on the stress extrapolation method. Source: Ref 5.7 More

Fig. 13.15 Examples of crack configurations and stress-intensity factors More

Fig. 4 Variation of time to failure with stress intensity, K , for three mill-annealed (MA) commercial α-β alloys of varying aluminum contents tested in 3.5% NaCl More

Fig. 8.26 Fatigue crack growth rate ( R = 0.1) versus stress-intensity factor at room temperature for A356.0-T6 aluminum alloy castings produced by various processes More

Fig. 8.27 Fatigue crack growth rate ( R = 0.5) versus stress-intensity factor at room temperature for A356.0-T6 aluminum alloy castings produced by various processes More