Khoun, L.De Oliveira, R.Michaud, V.Hubert, P.2011-02-152011-02-152011-02-15201110.1016/j.compositesa.2010.11.013https://infoscience.epfl.ch/handle/20.500.14299/64338WOS:000287288600007A comprehensive understanding of the development of residual strains in composite processing is essential to manufacture high quality composite parts. In this paper, the use of fibre Bragg grating (FBG) optical sensors was investigated to measure in situ the build-up of the process-induced strains in composite panels manufactured by resin transfer moulding. The FBG sensors, embedded in the composite laminate, successfully measured the evolution of the composite in-plane strains due to the temperature history. The sensors also captured a strain discontinuity during the cool-down related to the debonding of the composite from the mould. Finite element models were then proposed to simulate the strain development measured by the FBG sensors. Three different contact interactions between the tool and the laminate were investigated: no bonding, perfect bonding and frictional contact. The model using the frictional contact interaction described well the evolution of the measured strains. © 2010 Elsevier Ltd. All rights reserved.Polymer-matrix compositesResidual/internal stressProcess monitoringTool-part interactionTool-Part InteractionShape DistortionsResidual-StressesInternal-StressesThermoset ResinOptic SensorsSpring-InCureModelDeformationtext::journal::journal article::research article