PSI - Issue 35

Jarmil Vlach et al. / Procedia Structural Integrity 35 (2022) 132–140 Author name / Structural Integrity Procedia 00 (2019) 000 – 000

140

9

References

Šedek, J., Bělský , P., 2017. Numerical evaluation of barely visible impact damage in a carbon fibre-reinforced composite panel with shear loading, WIT Transactions on Engineering Sciences Vol. 116, WIT Press. EASA, 2010. European Aviation Safety Agency, AMC 20-29: Composite Aircraft structures, Annex II - AMC 20-29 to ED Decision 2010/003/R. FAA, 2016. Federal Aviation Administration , AAWG Structural Damage Capability Recommendation Document, Initial Revision. Růžek, R., Běhal, J., 2009 . Certification programme of airframe primary structure composite part with environmental simulation Int. J. of Fatigue, Volume 31(6), pp. 1073-1080. Kruse, T., Körwien, T., Růžek, 2016. R. Fatigue behaviour and damage tolerant design of composite bonded joints for aerospace ap-plication, Proceedings of the ECCM 17th European Conference on Composite Materials ECCM-17, Munich, Germany. Kruse, T., Körwien, T., Růžek, R., Hangx, R., Rans, 2017. C. Fatigue behaviour and damage tolerant design of bonded joints for aerospace application on Fibre Metal Laminates and composites, in Proc. of 29th Symposium of the International Committee on Aeronautical Fatigue, ICAF, Nagoya, Japan. Růžek, R., Tserpes, K., Karachalios, E., 2015. Compression after impact and fatigue behaviour of CFRP stiffened panels. International Journal of Structural Integrity, Vol. 6, Iss. 2., pp.176 – 193. Cagáň, J. , Pelant, J., Kyncl, M., Kadlec, M., Michalcová, L., 2019. Damage detection in carbon fiber – reinforced polymer composite via electrical resistance tomography with Gaussian anisotropic regularization. Structural Health Monitoring, vol. 18(5-6), s. 356-370. Kadlec, M., Růžek, R. , 2012. A Comparison of Laser Shearography and C-Scan for Assessing a Glass/Epoxy Laminate Impact Damage. Applied Composite Materials, Vol.19, No. 3-4, pp.393-407 IF 1,048. Růžek, R., Kadlec, M., Tserpes, K. and Karachalios, E. , 2017. Monitoring of compressive behaviour of stiffened composite panels using embedded fibre optic and strain gauge sensors, International Journal of Structural Integrity, Vol. 8 No. 1, pp. 134-150. Khan, U., A., 1999. Biman Bangladesh Airlines, Bangladesh. Non-destructive Testing Applications in Commercial Aircraft Maintenance. NDT.net - June 1999, Vol. 4 No. 6. Daniel, I., Ishai, O., 2006. Engineering mechanics of composite materials. Oxford university press, New York. Rektorys, K., 2003. Přehled užité matematiky II . Prometheus, Praha. Pierard, O., Friebel, C., Doghri, I., 2004. Mean-field homogenization of multi-phase thermo-elastic composites: a general framework and its validation. Composites Science and Technology 64, 1587 – 1603. Hvejsel, Ch., Lund, E., Stolpe, M., 2011. Optimization strategies for discrete multi-materials optimization. Structural and Multidisciplinary Optimization 44 (2), 149 – 163. Ye, F., Wang, H., 2017. A simple Python code for computing effective properties of 2D and 3D representative volume element under periodic boundary conditions. arXiv: 1703.03930. Wang, R., Chen, D., Zhu, M., & Xing, S., 2019. Dynamic effects of low-velocity impact on composite plates. IOP Conference Series: Materials Science and Engineering, 657(1), 9. Liao, B., & Liu, P., 2018. Finite element analysis of dynamic progressive failure properties of GLARE hybrid laminates under low-velocity impact. Journal of Composite Materials, 52(10), 1317-1330. Abaqus, 2017. Analysis User’s Manual. Version 2017, Dassault Systemes Simulia, Inc. Camanho, P.P., Dávila, C.G. & de Moura, M.F., 2003. Numerical simulation of mixed-mode progressive delamination in composite materials. Journal of Composite Materials, 37(16), pp. 1415 – 1438. Hashin, Z. & Rotem, A., 1973. A fatigue criterion for fiber-reinforced materials. Journal of Composite Materials, 7, pp. 448 – 464. Bouvet, Ch., Castanié, B., Bizeul, M. & Barrau, J.J., 2009. Low velocity impact modelling in laminate composite panels with discrete interface elements. International Journal of Solids and Structures, 46, pp. 2809 – 2821. Bouvet, C., Rivallant, S. & Barrau, J.J., 2012. Low velocity impact modeling in composite laminates capturing permanent indentation. Composites Science and Technology, 72(16), pp. 1977 – 1988. Shi, Y., Pinna, C. & Soutis, C., 2016. Low-velocity impact of composite laminates: damage evolution. Dynamic Deformation, Damage and Fracture in Composite Materials and Structures, ed. V. Silberchmidt, Woodhead Publishing, pp. 117 – 144.