Abstract
There have been several approaches used in the modelling of the process-induced deformations of composite parts developed so far. The most universal and most frequently used approach is the FEM modelling. In the scope of the FEM modelling several material models have been used to model the composite behaviour. In the present work two of the most popular material models: elastic and CHILE (cure hardening instantaneous linear elastic) are used to model the spring-in deformations of composite specimens and a structure fragment. The elastic model is more effective, whereas the CHILE model is considered more accurate. The results of the models are compared with each other and with the measured deformations of the real composite parts. Such a comparison shows that both models allow to predict the deformations reasonably well and that there is little difference between their results. This leads to a conclusion that the use of the simpler elastic model is a valid engineering practice.
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This research was carried out in the scope of Institute of Aviation statutory activity: ‘Manufacturing study of tail rotor blades and main rotor blades. Design and manufacturing of technologically advanced blades for ILX rotorcraft. Verification of tail rotor blade design technology.’
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Galińska, A. Material Models Used to Predict Spring-in of Composite Elements: a Comparative Study. Appl Compos Mater 24, 159–170 (2017). https://doi.org/10.1007/s10443-016-9519-y
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DOI: https://doi.org/10.1007/s10443-016-9519-y