Deformation and Fracture Mechanics of Engineering MaterialsUpdated to reflect recent developments in our understanding of deformation and fracture processes in structural materials. This completely revised reference includes new sections on isostress analysis, modulus of rupture, creep fracture micromechanicsms, and many more. |
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Page 45
... Tensile Strength MPa ( ksi ) 200-310 ( 30-45 ) 90-133 ( 13-20 ) 138 ( 20 ) 350-580 ( 50-80 ) 69 ( 10 ) 240-275 ( 35-40 ) " D. W. Richerson , Modern Ceramic Engineering , Marcel Dekker , Inc. New York ( 1992 ) . * Values corresponding to ...
... Tensile Strength MPa ( ksi ) 200-310 ( 30-45 ) 90-133 ( 13-20 ) 138 ( 20 ) 350-580 ( 50-80 ) 69 ( 10 ) 240-275 ( 35-40 ) " D. W. Richerson , Modern Ceramic Engineering , Marcel Dekker , Inc. New York ( 1992 ) . * Values corresponding to ...
Page 272
... tensile rather than a flexural loading condition ( recall Section 1.3 ) . Clearly , a tensile load generates the same stress across a com- ponent's entire cross - sectional area whereas flexural loading generates a maximum stress only ...
... tensile rather than a flexural loading condition ( recall Section 1.3 ) . Clearly , a tensile load generates the same stress across a com- ponent's entire cross - sectional area whereas flexural loading generates a maximum stress only ...
Page 543
... Tensile strength , MPa ( a ) Tensile strength , ksi 0 20 40 60 80 100 120 +400 +60 + 300 + 200 ± 100 Fatigue ratio 0.5 X X Fatigue ratio +40 0.35 X X +20 x x 200 400 Tensile strength , MPa ( b ) 600 800 Alternating fatigue strength ...
... Tensile strength , MPa ( a ) Tensile strength , ksi 0 20 40 60 80 100 120 +400 +60 + 300 + 200 ± 100 Fatigue ratio 0.5 X X Fatigue ratio +40 0.35 X X +20 x x 200 400 Tensile strength , MPa ( b ) 600 800 Alternating fatigue strength ...
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Common terms and phrases
addition alloy aluminum alloy applied stress associated ASTM atoms behavior brittle ceramics Chapter Charpy component composite crack extension crack growth crack length crack tip craze creep rate crystal curve cyclic decrease depends determined dislocation ductility elastic embrittlement engineering example factor failure fiber FIGURE flaw fracture mechanics fracture surface fracture toughness given grain boundaries hardening hydrogen increasing initial KIEAC lattice load maraging steels martensite material material's matrix Metals Park microstructure microvoid modulus notch Note occur oriented parameter particles phase plane plane-strain plastic deformation plastic zone plate polymer polymeric region relative Reprinted with permission result rupture sample screw dislocation Section shear stress shown in Fig solid solution specimen stacking fault energy steel alloys strain rate stress concentration stress field stress intensity stress level stress-strain stress-strain curve superalloys tensile stress test temperature thermal thickness toughening Trans transition temperature twinning values yield strength