Time-temperature behavior of carbon/epoxy laminates under creep loading

The time-temperature creep behavior of advanced composite laminates is herein determined through a comprehensive set of experiments and analytical modeling. A complete structureversusproperty relationship is determined through a wide range of temperature and applied stress levels at the three states of the composite: glassy, glass transition, and rubbery regions. Weibull, Eyring, Burger, and Findley models are employed to predict the experimental data and to better elucidate the material behavior. Experimental creep tests are carried out under ten min and two days aiming at calibrating fitting parameters, which are essential to validate short-term creep tests. The Weibull and Eyring models are more suitable for determining the time-temperature superposition (TTS) creep response in comparison to the Burger and Findley models.

Automated summary

This study investigates the time-temperature creep behavior of advanced composite laminates through experiments and analytical modeling, involving Weibull, Eyring, Burger, and Findley models. Experimental creep tests conducted in ten min and two days aim at calibrating fitting parameters essential for validating short-term creep tests. Weibull and Eyring models are found to be more suitable for determining the time-temperature superposition creep response compared to Burger and Findley models.