Search Results for axial stress

Fig. 9 Dependence of shear stress and mean axial stress on effective strain in fixed-end torsion tests at high temperatures. Source: Ref 12 More

Fig. 45 Ratio of maximum axial stress to maximum shear stress versus values of shear strain at failure for Inconel 600. Source: Ref 45 More

Fig. 21 Dependence of shear stress and mean axial stress on effective strain in fixed end torsion tests at high temperature. Source: Ref 16 More

Fig. 14(a) Smooth and notched axial stress fatigue data for commercially produced 2090-T86 extruded tee shapes. Extrusion thickness, 19 mm (0.75 in.); stress ratio ( R ), 0.1; specimen location, T-2. For notched specimen, theoretical stress concentration factor ( K t ) = 3. L, longitudinal More

Fig. 14(b) Smooth and notched axial stress fatigue data for commercially produced 2090-T81 plate. Plate thickness, 13 mm (0.5 in.); stress ratio ( R ), 0.1; specimen location, T-2. For notched specimen, theoretical stress concentration factor ( K t ) = 3. L, longitudinal orientation; LT, long More

Fig. 14(c) Smooth and notched axial stress fatigue data for commercially produced 2090-T83 sheet. Sheet thickness, 1.6 mm (0.063 in.); stress ratio ( R ), 0.1. For notched specimen, theoretical stress concentration factor ( K t ) = 3. L, longitudinal orientation; LT, long-transverse More

Fig. 24 Axial stress fatigue strength of 0.8 mm 2024, 7075, and clad sheet in air and seawater, R = 0. Source: Ref 33 More

Fig. 25 Comparison of axial-stress fatigue strengths of 0.032 in. aluminum alloy sheet in seawater and air. Source: Ref 33 More

Fig. 30 Axial stress in the 0° fiber next to the hole as a function of applied stress for the virgin and post-fatigued condition in [0/90] s SCS-6/Ti-15-3 laminates, V f = 0.355. The applied stress at which the 0° fiber stress reaches the fiber strength corresponds to the notched strength More

Fig. 12 (a) Axial stress and (b) displacement histories for the same cross section as Fig. 11 . Source: Ref 8 More

Fig. 36 (a) Axial stress accumulated in uniaxially constrained specimens during cooling of martensitic (9CrMo), bainitic (2CrMo), and austenitic (AISI 316) steels. Some experimental data are shown for yield strength (YS) of austenite in low-alloy steel. Adapted from Ref 47 . (b) Schematic More

Fig. 1 Smooth and notched axial stress fatigue data for 7050-T7451 plate, 1 to 6 in. (25 to 152 mm) thick, shown in relation to bands established for 7075 wrought products in T6 and T73 xx tempers More

Fig. 2 Smooth and notched axial stress fatigue data for 7050-T7452 hand forgings, 4 1 2 × 22 × 84 in. (144 × 559 × 2133 mm) More

Fig. 3 Smooth and notched axial stress fatigue data for 7050-T7651x extruded shapes, 1.161 in. (29.5 mm) thick More

Fig. 80 Analytical and numerical predictions of the maximum axial stress developed at the center of a 0.76 m (2.5 ft) ingot placed directly into a furnace at 1093 °C (2000 °F). The model stress predictions are compared to the material strength data corresponding to the predicted instantaneous More

Fig. 81 Analytical and numerical predictions of the maximum axial stress developed when a 0.76 m (2.5 ft) ingot is charged into a 649 °C (1200 °F) furnace for 10 h, after which the furnace temperature is raised at a rate of 140 °C/h (250 °F/h). The stresses are compared with material strength More

Fig. 3 Axial stress distribution at the symmetry plane of a necked portion of a tension specimen. Source: Ref 2 , 3 More

Fig. 2 Axial stress fatigue strength of 0.8 mm (0.032 in.) 2024, 7075, and clad sheet in air and seawater, R = 0. Source: Ref 4 More

Fig. 17 Comparison of axial-stress fatigue strengths of 0.812 mm (0.032 in.) aluminum alloy sheet in seawater and air. Source: Ref 4 More

Fig. 18 Ratio of axial-stress fatigue strength of aluminum alloy sheet in 3% NaCl solution to that in air. Specimens were 1.6 mm (0.064 in.) thick. More