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Influences of distributed propulsion system parameters on aerodynamic characteristics of a BLI-BWB UAV

Focusing on the aerodynamic characteristics of the blended wing body (BWB) aircraft with boundary layer ingestion(BLI) distributed propulsion system; the influences of propulsion system parameters under the condition of cruise and takeoff are studied. Firstly, based on the momentum source method (MS...

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Formato: Artigo
Idioma:Chinês
Publicado: EDP Sciences 2021-02-01
Series:Xibei Gongye Daxue Xuebao
Assuntos:
uav
distributed propulsion
boundary layer ingestion(bli)
blended wing body(bwb)
ducted fan
momentum source method
aerodynamic characteristics
lift-to-drag ratio
simulation
Acceso en liña:https://www.jnwpu.org/articles/jnwpu/full_html/2021/01/jnwpu2021391p17/jnwpu2021391p17.html
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