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 35
... applied to the composite . The fact that there are many discrete fibers in a given composite provides redundancy to the structure and precludes catastrophic fracture if one fiber were to contain a defect and , therefore , fracture ...
... applied to the composite . The fact that there are many discrete fibers in a given composite provides redundancy to the structure and precludes catastrophic fracture if one fiber were to contain a defect and , therefore , fracture ...
Page 114
... applied parallel to the basal plane or tensile loads applied parallel to the prism planes . The opposite is true for the case of c / a > √3 where twinning occurs when the prism plane is compressed or the basal plane extended . ( 0001 ) ...
... applied parallel to the basal plane or tensile loads applied parallel to the prism planes . The opposite is true for the case of c / a > √3 where twinning occurs when the prism plane is compressed or the basal plane extended . ( 0001 ) ...
Page 585
... applied cyclic load , PT , and preload , P1 , are both 5000 N , find the cyclic loads carried by the bolt and the ... applied load is equal to the preload . Furthermore , most of the applied load and the major portion of the load ...
... applied cyclic load , PT , and preload , P1 , are both 5000 N , find the cyclic loads carried by the bolt and the ... applied load is equal to the preload . Furthermore , most of the applied load and the major portion of the load ...
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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