Airfoil Selection Procedure, Wind Tunnel Experimentation and Implementation of 6DOF Modeling on a Flying Wing Micro Aerial Vehicle

Airfoil selection procedure, wind tunnel testing and an implementation of 6-DOF model on flying wing micro aerial vehicle (FWMAV) has been proposed in this research. The selection procedure of airfoil has been developed by considering parameters related to aerodynamic efficiency and flight stability...

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Detalles Bibliográficos
Autores principales: Shams, Taimur Ali, Shah, Syed Irtiza Ali, Javed, Ali, Hamdani, Syed Hossein Raza
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2020
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7345615/
https://www.ncbi.nlm.nih.gov/pubmed/32486120
http://dx.doi.org/10.3390/mi11060553

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7345615/
https://www.ncbi.nlm.nih.gov/pubmed/32486120
http://dx.doi.org/10.3390/mi11060553

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