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-Reference-Cited by-同舟云学术

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

Published:2017-02 Issue:1 Volume:30 Page:164-174
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

Koreanschi Andreea,Gabor Oliviu Sugar,Acotto Joran,Brianchon Guillaume,Portier Gregoire,Botez Ruxandra Mihaela,Mamou Mahmoud,Mebarki Youssef

Funder

Bombardier Aerospace, Thales Canada

The Consortium in Research and Aerospace in Canada

Natural Sciences and Engineering Research Council of Canada

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

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