Fig. 15 Typical load-displacement curve for a ductile polymer tested in uniaxial tension More

Fig. 23 Shear displacement of a spall prior to complete separation along the shear band. 330× More

Fig. 28 Correlation between crack-tip opening displacement (CTOD) and toughness. (a) Stretched-zone depth versus CTOD. (b) Stretched-zone width versus CTOD. (c) Stretched-zone width versus depth. Source: Ref 18 More

Fig. 20 Schematic illustration of loading modes for crack displacement: mode I (opening mode), mode II (in-plane shear), and mode III (out-of-plane shear, tearing) More

Fig. 9 Crack-tip opening displacement (CTOD) toughness, HSLA 50. δ, CTOD; δ c , CTOD fracture toughness, no significant stable crack extension, unstable fracture; δ e , elastic component of CTOD; δ m , CTOD fracture toughness, significant stable crack extension, plastic collapse; δ p , plastic More

Fig. 23 Displacement response versus time at impeller shaft (s = 1 second). More

Fig. 15 Typical load-displacement curve for a ductile polymer tested in uniaxial tension More

Fig. 15 The three modes of crack-surface displacement and associated loading: mode I (opening), mode II (sliding), and mode III (tearing) More

Fig. 43 Thermomechanical analysis (TMA) probe-displacement curves and extrapolated heat-distortion temperature values for two-ply unidirectional graphite composite. Source: Ref 88 More

Fig. 9 Load-displacement behavior of an impacted rubber-toughened polycarbonate box More

Fig. 19 Comparison of experimental force-displacement curves to simulations of the same elastomer-filled polypropylene at different temperatures More

Fig. 42 Nonlinear effects of cross-sectional collapse on load-displacement behavior More

Fig. 11 Damage following displacement of race. More

Fig. 8 Maximum shear stress as a function of displacement for two spring heights. The compressor that exhibited failures had a spring height of 25.0 mm. Lowering the compressor weight reduces the height, thus lowering the maximum stress as a function of lateral displacement. The fatigue bench More

Fig. 16 Vertical rise as a function of lateral displacement for compressor model #2. The linear regression shows a rise of 0.2566 mm for every 1 mm of lateral displacement. More

Fig. 10 (a) Fretting wear damage chart as a function of the applied displacement amplitude for a cylinder-on-flat contact. Quantification of the wear volume and crack length extension as a function of the fretting regime parameter, %GS. PSR, partial slip regime; MFR, mixed fretting regime; GSR More

Fig. 28 Correlation between crack-tip opening displacement (CTOD) and toughness. (a) Stretched-zone depth versus CTOD. (b) Stretched-zone width versus CTOD. (c) Stretched-zone width versus depth. Source: Ref 18 More

Fig. 20 Schematic illustration of loading modes for crack displacement: mode I (opening mode), mode II (in-plane shear), and mode III (out-of-plane shear, tearing) More

Fig. 14 Maximal resultant displacement (N = 6000 tr/min, α = 4°, m B e = 10 grcm) More

Fig. 16 Two different displacement boundary conditions for the mould: ( a ) fixing connecting holes in all three directions; ( b ) fixing connecting holes in out of plane (Y) direction only More