Semi-continuous approach for the modeling of thin woven composite panels applied to oblique impacts on helicopter blades |
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| Authors: | P Navarro J Aubry S Marguet J-F Ferrero S Lemaire P Rauch |
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| Affiliation: | 1. Université de Toulouse/ICA/ISAE, 10 av. E. Belin, 31055 Toulouse Cedex, France;2. Université de Toulouse/ICA/UPS, 118 Rte de Narbonne, 31062 Toulouse, France;3. Eurocopter Marignane/BDD – Aéroport Marseille P., 13725 Marignane, France;1. Department of Mechanical and Materials Engineering, Faculty of Engineering and Built Environment, Universiti Kebangsaan Malaysia, 43600 UKM Bangi, Selangor, Malaysia;2. Department Polytechnic Education, Ministry of Higher Education Malaysia, 62100 Putrajaya, Malaysia;1. School of Graduate Professional Studies, Penn State Great Valley, 30 East Swedesford Road, Malvern, PA 19355-1443, USA;2. Department of Mechanical Engineering, McGill University, 817 Sherbrook W, Montreal H3A 0C3, Canada;1. Unité de recherche de mécanique des solides, structures et développements technologiques, ESSTT, Université de Tunis, BP56, Bab Mnara 1008, Tunisia;2. LEMTA, Université de Lorraine, 2, Avenue de la Forêt de Haye, TSA 60604, BP 160, 54518 Vandoeuvre Cedex, France |
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| Abstract: | In aeronautics, passenger safety and reliability of structures are essential aspects. In the specific case of helicopters, blades are subjected to impact loadings. Modeling these phenomena continue to be difficult and experimental tests often replace the prediction. The following work will focus on the experimental and numerical study of an oblique impact on the skin of the blade. It is equivalent in a first approach to an impact on a sandwich panel made up of a foam core and a thin woven composite skin. The objectives are to identify the mechanisms of damage in the skin for this kind of loading and to develop a representative modeling of the chronology of damage adapted to the modeling of the complete structure. Thus, a semi-continuous F.E. explicit modeling has been developed. It relies on the development of a specific damageable element at the bundles scale. Satisfactory numerical results are obtained. They allow the identification of the damage mechanism of the woven skin. |
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