Skip to main navigation Skip to search Skip to main content

Design of a scalable trailing edge of morphing wings

  • Bing Li*
  • , Hefei Wang
  • , Gang Li
  • *Corresponding author for this work
  • Harbin Institute of Technology Shenzhen

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

A networking mechanism was designed based on scalable trailing edge to satisfy the requirements of morphing wings. By this way, we can increase the lift coefficient and the aerodynamic efficiency of the aircraft in the process of taking off and landing. We use Lagrange equations to set up the system dynamics model. Simulation results by Simulink and Fluent show that the whole system can realize the flexible curved transition and the system itself has good scalability. And it will have better improvement on the aerodynamic performance of the aircraft.

Original languageEnglish
Title of host publication2014 IEEE International Conference on Robotics and Biomimetics, IEEE ROBIO 2014
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages2378-2382
Number of pages5
ISBN (Electronic)9781479973965
DOIs
StatePublished - 20 Apr 2014
Externally publishedYes
Event2014 IEEE International Conference on Robotics and Biomimetics, ROBIO 2014 - Bali, Indonesia
Duration: 5 Dec 201410 Dec 2014

Publication series

Name2014 IEEE International Conference on Robotics and Biomimetics, IEEE ROBIO 2014

Conference

Conference2014 IEEE International Conference on Robotics and Biomimetics, ROBIO 2014
Country/TerritoryIndonesia
CityBali
Period5/12/1410/12/14

Fingerprint

Dive into the research topics of 'Design of a scalable trailing edge of morphing wings'. Together they form a unique fingerprint.

Cite this