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Transient aeroelastic responses and flutter analysis of a variable-span wing during the morphing process

  • Published:2013-12 Issue:6 Volume:26 Page:1430-1438
  • ISSN:1000-9361
  • Container-title:Chinese Journal of Aeronautics
  • language:en
  • Short-container-title:Chinese Journal of Aeronautics

Author:

Huang Ren,Qiu Zhiping

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference24 articles.

1. Morphing UAVs change the shape of warfare;Wilson;Aerosp Am,2004

2. Rodriguez AR. Morphing aircraft technology survey. AIAA-2007-1258; 2007.

3. A review of morphing aircraft;Barbarino;J Intell Mater Syst Struct,2011

4. A new flexible honeycomb structure and its application in structure design of morphing aircraft;Zhang;Acta Aeronaut Astronaut Sin,2011

5. System design and characteristics analysis of a variable-sweep and variable-span wing-body;Chen;Acta Aeronaut Astronaut Sin,2010

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1. Design and applications of morphing aircraft and their structures;Frontiers of Mechanical Engineering;2023-08-04

2. Aeroelasticity of Telescopic Morphing UAV Wing;AIAA AVIATION 2023 Forum;2023-06-08

3. A Review on Evolution of Aeroelastic Assisted Wing;International Journal of Aeronautical and Space Sciences;2023-04-14

4. On the Aeroelasticity of the Active Span and Passive Pitching Polymorphing Wing: Effect of Morphing Rate;Aerospace;2023-01-05

5. Structural modeling and dynamic analysis of the two-segment deployable beam system;International Journal of Mechanical Sciences;2022-11
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