Virtual testing of thermoplastic composites

Towards a hybrid simulation-physical testing pyramid

Conference Paper (2018)
Author(s)

B.H.A.H. Tijs (TU Delft - Aerospace Structures & Computational Mechanics, GKN Aerospace)

CS Lopes (IMDEA Materials Institute)

A. Turon (University of Girona)

C Bisagni (TU Delft - Aerospace Structures & Computational Mechanics)

J. Waleson (GKN Aerospace)

J.W. van Ingen (GKN Aerospace)

S.L. Veldman (GKN Aerospace)

Research Group
Aerospace Structures & Computational Mechanics
Copyright
© 2018 B.H.A.H. Tijs, CS Lopes, A. Turon, C. Bisagni, J. Waleson, J.W. van Ingen, S.L. Veldman
More Info
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Publication Year
2018
Language
English
Copyright
© 2018 B.H.A.H. Tijs, CS Lopes, A. Turon, C. Bisagni, J. Waleson, J.W. van Ingen, S.L. Veldman
Research Group
Aerospace Structures & Computational Mechanics
ISBN (electronic)
9781510896932
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Abstract

This paper summarizes the implementation of a Virtual Testing methodology in an industrial environment to predict the mechanical behaviour of composite material through the different scales of the conventional physical testing pyramid. A robust Virtual Test Lab allows for the generation of virtual allowables, while advanced interface models ensure accurate simulation of critical interfaces up to structural level. Hybrid simulation-physical testing approaches, that can support both conventional rapid sizing and high-fidelity analysis methods, have been applied during the development of a thermoplastic orthogrid fuselage shell and will be coupled with the manufacturing process though a virtual process chain for the development of a thermoplastic fuselage for the next generation aircraft.

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