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Modelling of small CFRP aerostructure parts for X-ray imaging simulation

Kristina Bliznakova (Technical University of Varna, Varna, Bulgaria)
Zacharias Kamarianakis (Department of Medical Physics, University of Patras, Patras, Greece)
Aris Dermitzakis (Department of Medical Physics, University of Patras, Patras, Greece)
Zhivko Bliznakov (Department of Medical Physics, University of Patras, Patras, Greece)
Ivan Buliev (Department of Electronics and Microelectronics, Technical University of Varna, Varna, Bulgaria)
Nicolas Pallikarakis (Department of Medical Physics, University of Patras, Patras, Greece)

International Journal of Structural Integrity

ISSN: 1757-9864

Article publication date: 12 August 2014

145

Abstract

Purpose

The purpose of this paper is to develop a realistic computational model of carbon fibre reinforced polymer (CFRP) structures dedicated for in-silico investigations of the use of X-ray-based imaging techniques as non-destructive testing (NDT) of CFRP parts.

Design/methodology/approach

CFRPs contain layers of carbon-fibres bundles within resin. Bundles’ orientation in the different layers is arranged with respect to each other at a well-defined primary direction. In the model, the bundle was simulated as a circular cylinder. The resulted model is a stack of layers of unidirectional bundles having orientation of 0°/90°/45°/−45°. Two CFRP structures were modelled: a flat CFRP part and a real shaped CFRP clip. A porous layer and non-carbon fibres were inserted within each model, respectively. X-ray projection images were generated with a dedicated simulation programme. Three setups were investigated: radiography, tomosynthesis and cone-beam CT (CBCT).

Findings

Results showed that porosity and non-carbon fibres were visible with all X-ray-based techniques. Tomosynthesis and CBCT, however, provide higher quality image of defects.

Practical implications

The CFRP computational model is a valuable tool in design, testing and optimization phase of X-ray-based imaging techniques for use in NDT of composite materials. Simulated images are generated within a short time; thus results from virtual optimization and testing are obtained very fast and at low cost.

Originality/value

An innovative computational model of CFRP structures, dedicated for X-ray imaging simulations, has been developed. The model is characterized by simplicity in its creation and realistic visual appearance of the produced X-ray images.

Keywords

Acknowledgements

The research leading to these results has gratefully received funding from the QUICOM Project of the European Union Seventh Framework Programme (FP7/2007- 2013), under Grant Agreement No. ACP2-GA-2012-314562.

Citation

Bliznakova, K., Kamarianakis, Z., Dermitzakis, A., Bliznakov, Z., Buliev, I. and Pallikarakis, N. (2014), "Modelling of small CFRP aerostructure parts for X-ray imaging simulation", International Journal of Structural Integrity, Vol. 5 No. 3, pp. 227-240. https://doi.org/10.1108/IJSI-02-2014-0009

Publisher

:

Emerald Group Publishing Limited

Copyright © 2014, Emerald Group Publishing Limited

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