Optimized Design and Test of Geometrically Nonlinear Static Aeroelasticity Model for High-Speed High-Aspect-Ratio Wing

Optimized Design and Test of Geometrically Nonlinear Static Aeroelasticity Model for High-Speed High-Aspect-Ratio Wing

Large transport aircraft tend to adopt a wing layout with a high aspect ratio and swept-back angle due to the requirement of a high lift-to-drag ratio. Composite material is typically employed to ensure the light weight of the structure, causing serious static aeroelasticity problems to the aircraft...

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Bibliographic Details
Main Authors: Xing Li, Wei Qian, Ling Xiao, Xinyu Ai, Jun Liu
Format: Article
Language:English
Published: MDPI AG 2024-12-01
Series:Aerospace
Subjects:
aeroelastic
airplane design
optimization for design
wind tunnel test
Online Access:https://www.mdpi.com/2226-4310/11/12/1015
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