Crossmark

Optimization and design of an aircraft's morphing wing-tip demonstrator for drag reduction at low speeds, Part II - Experimental validation using Infra-Red transition measurement from Wind Tunnel tests

Crossref DOI link: https://doi.org/10.1016/j.cja.2016.12.018

Published Print: 2017-02

Update policy: https://doi.org/10.1016/elsevier_cm_policy

Authors

Koreanschi, Andreea

Gabor, Oliviu Sugar

Acotto, Joran

Brianchon, Guillaume

Portier, Gregoire

Botez, Ruxandra Mihaela

Mamou, Mahmoud

Mebarki, Youssef
Funding

Funding for this research was provided by:

Bombardier Aerospace, Thales Canada

The Consortium in Research and Aerospace in Canada

Natural Sciences and Engineering Research Council of Canada
License Information

Text and Data Mining valid from 2017-02-01

Text and Data Mining valid from 2017-02-01

Version of Record valid from 2016-12-20
More Information

This article is maintained by: Elsevier

Article Title: Optimization and design of an aircraft's morphing wing-tip demonstrator for drag reduction at low speeds, Part II - Experimental validation using Infra-Red transition measurement from Wind Tunnel tests

Journal Title: Chinese Journal of Aeronautics

CrossRef DOI link to publisher maintained version: https://doi.org/10.1016/j.cja.2016.12.018

Content Type: article

Copyright: © 2017 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd.

Document is current

Any future updates will be listed below