UAV Wing leading edge crashworthiness behaviour under bird strike events: The added value of CF/PA additive solutions versus traditional metallic wing structures-Reference-Cited by-同舟云学术

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UAV Wing leading edge crashworthiness behaviour under bird strike events: The added value of CF/PA additive solutions versus traditional metallic wing structures

Published:2024-10 Issue: Volume:15 Page:100506
ISSN:2666-6820
Container-title:Composites Part C: Open Access
language:en
Short-container-title:Composites Part C: Open Access

Author:

Battaglia Miriam^ORCID,Acanfora Valerio,Riccio Aniello

Publisher

Elsevier BV

Reference37 articles.

1. Validation of available approaches for numerical bird strike modeling tools;Lavoie;Internat. Rev. Mech. Eng.,2007

2. Bird strike damage & windshield bird strike;Dennis,2009

3. Crashworthiness of wing leading edges under bird impact event;Di Caprio;Compos. Struct.,2019

4. Crashworthiness of a composite wing section: numerical investigation of the bird strike phenomenon by using a coupled eulerian–Lagrangian approach;Saputo;J. Mater. Eng. Perform.,2019

5. Failure modeling of composite wing leading edge under bird strike;Long;Compos. Struct.,2021

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