Static aeroelastic analysis of very flexible wings coupled with distributed propellers

Static aeroelastic analysis of very flexible wings coupled with distributed propellers

Distributed propellers are widely used as propulsion for high-aspect-ratio long-endurance UAVs, and their load and slipstream will change the structural and aerodynamic characteristics of the wing, making geometric nonlinear effects more prominent. To address the aeroelastic interference of distribu...

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Bibliographic Details
Main Authors: WU Xuan, ZHOU Zhou, WANG Zhengping
Format: Article
Language:zho
Published: EDP Sciences 2023-12-01
Series:Xibei Gongye Daxue Xuebao
Subjects:
distributed propellers
slipstream
flexible wing
geometric nonlinearity
static aeroelasticity
Online Access:https://www.jnwpu.org/articles/jnwpu/full_html/2023/06/jnwpu2023416p1044/jnwpu2023416p1044.html

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https://www.jnwpu.org/articles/jnwpu/full_html/2023/06/jnwpu2023416p1044/jnwpu2023416p1044.html

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