Creep and Fatigue in Polymer Matrix Composites (Woodhead by R M Guedes

By R M Guedes

Creep is the tendency of fabrics to deform while subjected to long term pressure, fairly whilst uncovered to warmth. Fatigue phenomena take place whilst a fabric is subjected to cyclic loading, inflicting harm which could growth to failure. either are serious components within the long term functionality and reliability of fabrics comparable to polymer matrix composites, that are usually uncovered to those varieties of stresses in civil engineering and different functions. this significant e-book studies the newest study in modeling and predicting creep and fatigue in polymer matrix composites. the 1st a part of the booklet reports the modeling of viscoelastic and viscoplastic habit as a fashion of predicting functionality and repair existence. half discusses thoughts for modeling creep rupture and failure. the ultimate a part of the publication addresses methods of checking out and predicting long term creep and fatigue in polymer matrix composites.

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Extra info for Creep and Fatigue in Polymer Matrix Composites (Woodhead Publishing in Materials)

Sample text

The specimens were subjected to a constant stress σ at time t0. During step 1 for a time interval (t1 – t0), we observe an immediate elastic deformation of the Maxwell spring (at time t0) corresponding to diagram (a) in Fig. 14, followed by a slower extension of the Voigt element, (b); finally the Maxwell dashpot begins to move, corresponding to inelastic deformation, also shown in diagram (b). In step 2, the specimen is quickly returned to zero load at time t1. The Maxwell spring immediately returns to zero extension as shown by diagram (c).

Lai J, Bakker A (1995), Analysis of the Nonlinear Creep of High-Density Polypropylene, Polymer, 36, 93–99. Leaderman H (1943), Elastic and Creep Properties of Filamentous Materials and Other High Polymers, The Textile Foundation, Washington, DC. Ma C C M, Tai N H, Wu S H, Lin S H, Wu J F, Lin, J M (1997), Creep Behavior of CarbonFiber-Reinforced Polyetheretherketone (PEEK) Laminated Composites, Composites Part B, 28, 407–417. Mohan R, Adams D F (1985), Nonlinear creep-recovery response of a polymer matrix and its composites, Experimental Mechanics, 25, 262–271.

Thus only 37% of the initial stress remains at t = tR. 4 The Voigt or Kelvin model The Voigt model is shown in Fig. 11 where the spring element and dashpot element are connected in parallel. 38] Creep The solution of Eq. 11 The Voigt or Kelvin model. As shown in Fig. 11, the strain described by Eq. 39 increases with a decreasing rate and approaches asymptotically the value of σ0/E when t tends to infinity. The response of this model to an abruptly applied stress is that the stress is at first carried entirely by the viscous element.

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