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Fig. 24 Micrographs showing the buckling within a failed bucket. A sink mark within the sidewall is also illustrated. More

Fig. 7 Action of turret and drums within a centrifugal barrel finishing machine More

Fig. 3 Action of media and parts within a rotating barrel More

Fig. 1 Action of media and parts within a rotating barrel More

Fig. 11 (a) Customer specifications of hardenability within an H-band for SAE 8620H. (b) Jominy curve for finished heat. Source: Ref 19 More

Fig. 27 Current density distribution within coil turns in a multiturn coil. (Turn numbers correspond to those in Fig. 26 .) Source: Ref 26 More

Fig. 4 Thermal profile within an induction melter More

Fig. 4 Currents flowing within a thin sheath at the surface of a superconductor preventing the external applied magnetic field from entering the bulk. The thickness of the current sheath, and the distance over which the magnetic field decays is called the penetration length (λ). More

Fig. 21 Cross section of a Cu/NbTi strand continuously coextruded within high-purity aluminum with rectangular dimensions (2.1 × 3.2 mm, or 0.083 × 0.126 in.). Courtesy of IGC Advanced Superconductors Inc. More

Fig. 12 Variation of hardenability within a heat of 4028 steel More

Fig. 19 Isothermal growth of a graphite spheroid within an austenite shell and growth of the shell with a smooth interface. (a) Growth of spheroidal graphite in contact with melt. (b) Envelopment by austenite. (c) Growth of spheroidal graphite within the austenite shell. Source: Ref 24 More

Fig. 28 Cam that was blanked and pierced in a compound die within an envelope tolerance of 0.13 mm (0.005 in.) total indicator reading. Dimensions given in inches More

Fig. 6 Increase in the range of values within a subset (increase in R ). Values of X ¯ remain the same. More

Fig. 29 Alpha case. (a) Alpha layer (within the parallel vertical lines) developed at the surface of a sand casting. (b) Detail. Source: Ref 62 More

Fig. 41 Bracket with unbalanced shape that was held within bending tolerances by restriking and by extra-close tolerances on some parts of bending dies. Dimensions given in inches More

Fig. 19 Different dislocation arrangements within a single grain of copper. Δε pl /2 = 5 × 10 −4 , N ≈ 10 5 . Source: Ref 101 More

Fig. 26 Changes of plastic strain rate within each cycle. Source: Ref 146 More

Fig. 4 Fe-1.86C alloy color etched with 2% nital to reveal plate martensite within austenite grains and ledeburite in the grain boundaries. 500×. (A.O. Benscoter) More

Fig. 22 Location of minimum and maximum temperature points within the finite length cylinder at the end of time-optimal heating process: (a–c) for ε = ε min ( 1 ) , and (d–f) for ε = ε * . More

Fig. 24 Location of minimum and maximum temperature points within the finite length cylinder at the end of the time-optimal heating process for ε = ε * * = ε min ( 2 ) More