Aerodynamic Design, Analysis and Validation of a Small Blended-Wing-Body Unmanned Aerial Vehicle

This paper describes the aerodynamic design and assessment of a blended-wing–body (BWB) configuration under the distributed electric propulsion (DEP) installation constraints. The aerodynamic design rationale and process is described, as well as how the DEP system is considered and simplified in the...

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Detalhes bibliográficos

Principais autores:	Kelei Wang, Zhou Zhou
Formato:	Artigo
Idioma:	Inglês
Publicado em:	MDPI AG 2022-01-01
coleção:	Aerospace
Assuntos:	blended-wing–body configuration distributed electric propulsion wind tunnel test aerodynamic characteristics optimization design
Acesso em linha:	https://www.mdpi.com/2226-4310/9/1/36
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