Nonlinear aeroservoelastic analysis of a supersonic aircraft with control fin free-play by component mode synthesis technique-Reference-Cited by-同舟云学术

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Nonlinear aeroservoelastic analysis of a supersonic aircraft with control fin free-play by component mode synthesis technique

Published:2021-02 Issue: Volume:493 Page:115835
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Tian Wei^ORCID,Gu Yingsong,Liu Hao,Wang Xiaochen^ORCID,Yang Zhichun,Li Yueming,Li Ping

Funder

China Postdoctoral Science Foundation

National Natural Science Foundations of China

Natural Science Basic Research Plan in Shaanxi Province of China

Overseas Expertise Introduction Project for

Discipline Innovation

111 Project

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference56 articles.

1. Nonlinear modal aeroservoelastic analysis framework for flexible aircraft;Wang;AIAA J.,2016

2. Nonlinear aeroelastic characteristics of an all-movable fin with freeplay and aerodynamic nonlinearities in hypersonic flow;Tian;Int. J. Non-Linear. Mech.,2019

3. Nonlinear open-/closed-loop aeroelastic analysis of airfoils via Volterra series;Marzocca;AIAA J.,2004

4. Implications of time-delayed feedback control on limit cycle oscillation of a two-dimensional supersonic lifting surface;Yu;J. Sound. Vib.,2007

5. Nonlinear stability analysis of control surface flutter with freeplay effects;Gordon;J. Aircraft.,2008

Cited by 20 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. L1 adaptive aeroelastic control of an unsteady flapped airfoil in the presence of unmatched nonlinear uncertainties;Journal of Sound and Vibration;2024-05

2. Nonlinear aeroelastic analysis of a twin-tail boom UAV with rudder freeplay nonlinearities;Chinese Journal of Aeronautics;2024-04

3. Overview of Computational Methods to Predict Flutter in Aircraft;Journal of Applied Mechanics;2024-01-29

4. Wind Tunnel Tests of an Aeroelastic Model with Multiple Control Surface Freeplay Nonlinearities;AIAA SCITECH 2024 Forum;2024-01-04

5. Nonlinear Aeroelastic Study of an All-Movable Horizontal Tail with Multiple Free-Plays and Angle of Attack;Lecture Notes in Electrical Engineering;2024

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