## Fatigue of engineering plastics |

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Page 198

At a critical axial

this point, crazing was observed. With repeated stress-strain cycling, they

obtained curves resembling those shown in Fig. 5.9. As might be expected,

crazing ...

At a critical axial

**tensile**stress, damping became dependent on the amplitude; atthis point, crazing was observed. With repeated stress-strain cycling, they

obtained curves resembling those shown in Fig. 5.9. As might be expected,

crazing ...

Page 200

Thus, with ABS, the

losses, while with HIPS (after ~ 60 cycles), increasingly higher energy losses

were shown in the

secant ...

Thus, with ABS, the

**tensile**and compressive half-cycles exhibited similar energylosses, while with HIPS (after ~ 60 cycles), increasingly higher energy losses

were shown in the

**tensile**than in the compressive half-cycle. Moreover, thesecant ...

Page 268

A.l Longitudinal

Matrix shear failure known called interlaminar, shear Failure response (a) Matrix

splitting (b) ...

A.l Longitudinal

**tensile**failure modes: (a). (a) Matrix compressive failure (a)Matrix shear failure known called interlaminar, shear Failure response (a) Matrix

**tensile**failure (b) Matrix**tensile**failure. constituent debonding. and/or fibersplitting (b) ...

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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