Fatigue of engineering plastics |
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Page 17
As the stress rises further, the response (region II) becomes nonlinear; energy is
still recoverable on release of the ... In any case, under the influence of an
applied stress, the energy barriers to segmental mobility are presumably
decreased (cf.
As the stress rises further, the response (region II) becomes nonlinear; energy is
still recoverable on release of the ... In any case, under the influence of an
applied stress, the energy barriers to segmental mobility are presumably
decreased (cf.
Page 20
As mentioned above, development of a craze is clearly linked to the dilatational (
hydrostatic) component of the applied stress [75, 101], a relationship originally
put forward for cavitation in other materials by Bridgman [103]. At the same time, ...
As mentioned above, development of a craze is clearly linked to the dilatational (
hydrostatic) component of the applied stress [75, 101], a relationship originally
put forward for cavitation in other materials by Bridgman [103]. At the same time, ...
Page 138
Note that the computation of cyclic life depends on knowledge of such variables
as the applied stress range, the stress intensity calibration factor Y, the material
constants A and m and the starting and final flaw sizes. In practical situations ...
Note that the computation of cyclic life depends on knowledge of such variables
as the applied stress range, the stress intensity calibration factor Y, the material
constants A and m and the starting and final flaw sizes. In practical situations ...
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Contents
Fatigue Crack Propagation | 74 |
Fatigue Fracture Micromechanisms in Engineering Plastics | 146 |
Composite Systems | 184 |
Copyright | |
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Common terms and phrases
adhesive amplitude ASTM ASTM STP Beardmore Bucknall carbon cfrp component Composite Materials composites constant crack growth rates crack length crack tip craze crystalline cyclic loading da/dN decrease deformation discontinuous growth bands discussed ductile effect elastic elastic modulus energy epoxy fatigue behavior fatigue crack growth fatigue crack propagation fatigue failure fatigue fracture fatigue tests FCP behavior FCP rates fibers flaw fracture mechanics fracture surface fracture toughness frequency sensitivity hysteresis hysteretic heating increase J. A. Manson Kambour laminates loading cycles M. D. Skibo material matrix mean stress modulus molecular weight notched nylon 66 plastic zone PMMA polyacetal polycarbonate polymeric solids polystyrene properties PVDF R. W. Hertzberg Rabinowitz rubber S-N curve samples Section semicrystalline shown in Fig specimen spherulite static stress intensity factor stress level striation studies temperature rise tensile test frequency thermal failure tion toughening unnotched values viscoelastic yield strength