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Research on Conceptual Design Method and Propulsive/Aerodynamic Coupling Characteristics of DEP STOL UAV

This paper establishes an analytical model for component mass, takeoff weight, and performance constraints of distributed electric propulsion (DEP) propeller-driven short takeoff and landing (STOL) unmanned aerial vehicles (UAV), and develops a conceptual design method considering propulsive/aerodyn...

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Principais autores: Xin Zhao, Zhou Zhou, Kelei Wang, Han Wang, Xu Li
Formato: Artigo
Idioma:Inglês
Publicado em: MDPI AG 2025-05-01
coleção:Drones
Assuntos:
distributed electric propulsion (DEP)
short takeoff and landing (STOL)
propulsive/aerodynamic coupling effects
conceptual design method
lift-enhancement
Acesso em linha:https://www.mdpi.com/2504-446X/9/5/363
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