Numerical simulation and wind tunnel tests investigation and validation of a morphing wing-tip demonstrator aerodynamic performance-Reference-Cited by-同舟云学术

Numerical simulation and wind tunnel tests investigation and validation of a morphing wing-tip demonstrator aerodynamic performance

Published:2016-06 Issue: Volume:53 Page:136-153
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Şugar Gabor Oliviu,Koreanschi Andreea,Botez Ruxandra Mihaela,Mamou Mahmoud,Mebarki Youssef

Funder

Bombardier

Thales Canada

NSERC

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference43 articles.

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4. P. Gamboa, P. Alexio, J. Vale, F. Lau, A. Suleman, Design and testing of a morphing wing for an experimental UAV, RTO-MP-AVT-146, Neuilly-sur-Seine, France, 2007.

5. Aero-structural optimization and performance evaluation of a morphing wing with variable span and camber;do Vale;J. Intell. Mater. Syst. Struct.,2011

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