Design, Manufacturing, and Testing of a New Concept for a Morphing Leading Edge using a Subsonic Blow Down Wind Tunnel

This paper presents the design and wind tunnel test results of a wing including a morphing leading edge for a medium unmanned aerial vehicle with a maximum wingspan of 5 m. The design of the morphing leading edge system is part of research on the design of a morphing camber system. The concept prese...

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Detalles Bibliográficos
Autores principales: Communier, David, Le Besnerais, Franck, Botez, Ruxandra Mihaela, Wong, Tony
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2019
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6963326/
https://www.ncbi.nlm.nih.gov/pubmed/31810231
http://dx.doi.org/10.3390/biomimetics4040076

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6963326/
https://www.ncbi.nlm.nih.gov/pubmed/31810231
http://dx.doi.org/10.3390/biomimetics4040076

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