Modelling the Dynamic Response of a Morphing Wing with Active Winglets

Author:

Ameri Nima1,Lowenberg Mark1,Friswell Michael1

Affiliation:

1. Univeristy of Bristol

Publisher

American Institute of Aeronautics and Astronautics

Cited by 12 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. Research on deployment process of gravitational airdrop UAV;Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University;2022-06

2. Trailing Edge Tabs on Folding Wingtips (FWTs) for Aircraft Roll Control;AIAA SCITECH 2022 Forum;2022-01-03

3. Sliding mode control design for oblique wing aircraft in wing skewing process;Chinese Journal of Aeronautics;2019-02

4. Gust and Ground Loads Integration for Aircraft Landing Loads Prediction;58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2017-01-05

5. Effect of Symmetric & Asymmetric Span Morphing on Flight Dynamics;AIAA Atmospheric Flight Mechanics Conference;2014-01-10

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