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. |
From inside the book
Results 1-3 of 3
Page 333
... ( MPaVm ) Designation Product L - T T - L S - T 2014 - T651 127 mm plate 22.9 22.7 20.4 7075 - T651 45 mm plate 29.7 24.5 16.3 7079 - T651 45 mm plate 29.7 26.3 17.8 7075 - T6511 90 x 190 extruded bar 34.0 22.9 20.9 7178 - T6511 90 x 190 ...
... ( MPaVm ) Designation Product L - T T - L S - T 2014 - T651 127 mm plate 22.9 22.7 20.4 7075 - T651 45 mm plate 29.7 24.5 16.3 7079 - T651 45 mm plate 29.7 26.3 17.8 7075 - T6511 90 x 190 extruded bar 34.0 22.9 20.9 7178 - T6511 90 x 190 ...
Page 490
... MPaVm kg / mm3 / 2 MPa Vm kg / mm3 / 2 MPaVm kg / mm3 / 2 0.1 10.4 33.5 9.4 30.2 5.1 16.3 0.2 11.2 36 8.9 28.8 5.2 16.7 0.3 12.1 39 8.5 27.3 5.2 16.9 0.4 13 42 7.8 25.2 5.1 16.6 0.5 14.3 46 7.1 23 5.0 16.1 " AKeff in 2024 - T3 aluminum ...
... MPaVm kg / mm3 / 2 MPa Vm kg / mm3 / 2 MPaVm kg / mm3 / 2 0.1 10.4 33.5 9.4 30.2 5.1 16.3 0.2 11.2 36 8.9 28.8 5.2 16.7 0.3 12.1 39 8.5 27.3 5.2 16.9 0.4 13 42 7.8 25.2 5.1 16.6 0.5 14.3 46 7.1 23 5.0 16.1 " AKeff in 2024 - T3 aluminum ...
Page 572
... MPaVm , a lower bound stress range is found to be o = 455-540 MPa It is concluded that the actual stress range for failure was 455-540 actual < 615-730 MPa It is seen that the failure stress is approximately equal to the material yield ...
... MPaVm , a lower bound stress range is found to be o = 455-540 MPa It is concluded that the actual stress range for failure was 455-540 actual < 615-730 MPa It is seen that the failure stress is approximately equal to the material yield ...
Other editions - View all
Common terms and phrases
alloy aluminum alloy American Society applied stress associated ASTM STP atoms behavior brittle Burgers vector Chapter Charpy component crack growth rate crack length crack tip craze crystal crystalline cycles decreasing depends ductility effect elastic embrittlement engineering environment assisted cracking example failure FIGURE flaw fracture mechanics fracture surface fracture toughness given grain boundary hydrogen initial KIEAC lattice load Materials from copyright metallurgical microstructure modulus MPa Vm notch occur orientation parameter plane strain plane stress plastic deformation plastic zone plate polymer properties R. W. Hertzberg region relationship relative Reprinted with permission response result sample screw dislocation Section sensitivity shear stress shown in Fig slip plane slip systems specimen stacking fault energy strain hardening strain rate stress concentration stress intensity factor stress level stress-strain curve striation Table tensile test temperature Testing and Materials texture thickness Trans transition temperature twin values yield strength