Aerodynamic Analysis of Camber Morphing Airfoils in Transition via Computational Fluid Dynamics

In this paper, the authors analyze an important but overlooked area, the aerodynamics of the variable camber morphing wing in transition, where 6% camber changes from 2% to 8% using the two airfoil configurations: NACA2410 and NACA8410. Many morphing works focus on analyzing the aerodynamics of a pa...

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Detalles Bibliográficos
Autores principales: Jo, Bruce W., Majid, Tuba
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2022
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9149911/
https://www.ncbi.nlm.nih.gov/pubmed/35645179
http://dx.doi.org/10.3390/biomimetics7020052

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9149911/
https://www.ncbi.nlm.nih.gov/pubmed/35645179
http://dx.doi.org/10.3390/biomimetics7020052

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