Experimental and Numerical Studies on Static Aeroelastic Behaviours of a Forward-Swept Wing Model
Author:
Affiliation:
1. Institute of Structural Dynamics and Control, School of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, China
2. High Speed Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China
Abstract
Funder
National Natural Science Foundation of China
Publisher
Hindawi Limited
Subject
Mechanical Engineering,Mechanics of Materials,Geotechnical Engineering and Engineering Geology,Condensed Matter Physics,Civil and Structural Engineering
Link
http://downloads.hindawi.com/journals/sv/2021/5535192.pdf
Reference37 articles.
1. Introduction to Aircraft Aeroelasticity and Loads
2. Nonlinear vibration isolation via a circular ring
3. Vibration isolation and energy harvesting integrated in a Stewart platform with high static and low dynamic stiffness
4. Nonlinear large deflection theory with modified aeroelastic lifting line aerodynamics for a high aspect ratio flexible wing;N. Nguyen
5. Nonlinear Static Aeroelastic and Trim Analysis of Highly Flexible Joined-Wing Aircraft
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