Parametric study of a SPH high velocity impact analysis – A birdstrike windshield application

Author:

Grimaldi A.,Sollo A.,Guida M.,Marulo F.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference15 articles.

1. European Aviation Safety Agency. CS-25.631 Bird strike damage – certification specifications and acceptable means of compliance for large aeroplanes. Annex to ED decision 2011/004/R.

2. Federal Aviation Administration. Dept. of transportation, “Bird Strike Damage”. Part 25 Airworthiness Standards: Transport Category Airplanes, Sec. 25.631, Washington, DC; 2003.

3. Ubels L, Johnson A, Gallard J, Sunaric M. Design and testing of a composite birdstrike resistant leading edge. Tech. rep., National Aerospace Laboratory NLR, Amsterdam, The Netherlands; 2003.

4. Modelling of birdstrike on an aircraft wing leading edge made from fibre metal laminates – Part 2: modelling of impact with SPH bird model;McCarthy;Appl Compos Mater,2004

5. SPH–Lagrangian study of bird impact on leading edge wing;Guida;Compos Struct,2011

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