Wind Tunnel Test of a Morphing Wingtip Leading Edge

Ronald Cheung, Christopher Wales, Jonathan Cooper, Srinivas Vasista, Johannes Riemenschneider, Bram van de Kamp, Hans Peter Monner

Research output: Chapter in Book/Report/Conference proceedingConference Contribution (Conference Proceeding)

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Abstract

A full scale morphing wing tip demonstrator with a droop-nose adaptive morphing wingtip was wind tunnel tested as part of the European FP7 project NOVEMOR. This demonstrator features a flexible fiberglass skin and an aluminium internal compliant mechanism. The tests were carried out to assess the performance of compliant mechanism and skin under aerodynamic loading. The results show that strains in the mechanism are mainly from the actuation showing adequate stiffness in the mechanism. In addition to strains, pressure data was taken to determine aerodynamic loading. The Finite element and computational fluid dynamics simulations performed showed good agreement with the experimental values.
Original languageEnglish
Title of host publicationInternational Forum on Aeroelasticity and Structural Dynamics (IFASD 2015)
Subtitle of host publicationProceedings of a meeting held 28 June - 2 July, 2015, Saint Petersburg, Russia
PublisherCentral Aerohydrodynamic Institute (TsAGI)
Number of pages16
ISBN (Print)9781510821828
Publication statusPublished - 28 Jun 2015

Keywords

  • morphing wing
  • droop-nose
  • compliant mechanism

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