Fig. 22.24 (a) Normal stress distribution for original punch geometry. (b) Normal stress distribution for modified punch geometry (A, face; B, lower punch corner; C, cone angle; D, fillet radius; E, edge) [ Lange et al., 1992b ] More

Fig. 12 Schematic of (a) ductile tearing along plane normal to normal stress and (b) zig-zag path of void sheet fracture along shear planes. Source: Ref 3 More

Fig. 2.57 Variation of critical shear stress for flow and of critical normal stress for fracture with temperature. Source: Ref 2.4 More

Fig. 7 The influence of the direction of principal normal stress on the shape of dimples formed by microvoid coalescence. Transmission electron microscopic (TEM) fractographs are phase-contrast (p-c) replicas of fracture areas. Source: Ref 2 More

Fig. 16 Influence of direction of principal normal stress on the shape of dimples formed by microvoid coalescence. TEM, transmission electron microscopy. Source: Ref 9 More

Fig. 2.16 Free-body diagrams showing orientation of normal stresses and shear stresses in a shaft under simple (a) tension, (b) torsion, and (c) compression loading, and the single-overload fracture behavior of ductile and brittle materials More

Fig. 5.11 Normalized stress-intensity factors for single through-thickness cracks emanating from a straight lug subjected to a pin loading applied in the 0° loading direction. Source: Ref 5.15 More

Fig. 5.12 Normalized stress-intensity factors for single through-thickness cracks emanating from a tapered lug subjected to a pin loading applied in the 0° loading direction. Source: Ref 5.15 More

Fig. 5.13 Normalized stress-intensity factors for single through-thickness cracks emanating from a tapered lug subjected to a pin loading applied in the 180° loading direction. Source: Ref 5.15 More

Fig. 5.14 Normalized stress-intensity factors for single through-thickness cracks emanating from a tapered lug subjected to a pin loading applied in the −45° loading direction and its reversed direction, R o / R i = 2.25. Source: Ref 5.15 More

Fig. 5.15 Normalized stress-intensity factors for single through-thickness cracks emanating from a tapered lug subjected to a pin loading applied in the −90° loading direction and its reversed direction, R o / R i = 2.25. Source: Ref 5.15 More

Fig. A1.12 Diagram for calculating resolved shear and resolved normal stresses More

Fig. 2 Crack opening displacement modes. (a) Caused by stress normal to the crack face; considered most serious of loading modes, because K Ic < K IIc , K IIIc; therefore, design usually based on K I , K Ic . (b) Shearing or forward shear; caused by in-plane shear stress; crack More

Figure 13.20: Experimentally determined normal and shear stress distributions. More

Fig. 31 Stress-strain curves for tests conducted at “normal” and “zero” strain rates More

Fig. 5.8 The general state of stress and its equivalent system based on shear and normal stresses on the octahedral formed by the eight octahedral planes. (a) Principal planes with one octahedral plane shown by the shaded area. (b) Normal stresses on the eight octahedral planes. (c) Shear More

Fig. 1.31 Schematic diagram of time to failure vs. applied stress, σ, normalized to the yield strength σ y for stress corrosion More

Fig. 6 Complete engineering stress-strain curve showing the normally considered tensile region (upper right) and the often neglected compression region (lower left) More

Fig. 4 Variation of minimum creep rate with stress for a normalized and tempered 1.25Cr-0.50Mo steel. T and I denote transgranular and intergranular failure, respectively. Source: Ref 4 More

Fig. 28 Schematic diagram of time to failure versus applied stress, σ, normalized to the yield strength σ y for stress corrosion More