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

Author(s)

Ornaghi Jr, Heitor L. ; Almeida, Jr., Jose Humberto S. ^[1] ; Monticeli, Francisco M. ^[2] ; Neves, Roberta M. ^[3] ; Cioffi, Maria Odila H. ^[2]

Affiliation

^[1] Aalto Univ, Dept Mech Engn, Espoo 02150 - Finland

^[2] Ornaghi Jr, Jr., Heitor L., Sao Paulo State Univ, Dept Mat & Technol, BR-12516410 Guaratingueta, SP - Brazil

^[3] Univ Fed Rio Grande do Sul, PPGE3M, Av Bento Goncalves 9500, Porto Alegre, RS - Brazil

• Document type: Journal article
• Source: MECHANICS OF TIME-DEPENDENT MATERIALS; v. 25, n. 4, p. 601-615, DEC 2021.
• Web of Science Citations: 6

Abstract

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. (AU)

• FAPESP's process: 06/02121-6 - Composite processing by RTM
• Grantee: Maria Odila Hilário Cioffi
• Support Opportunities: Research Grants - Young Investigators Grants