A new non-linear vortex lattice method: Applications to wing aerodynamic optimizations-Reference-Cited by-同舟云学术

A new non-linear vortex lattice method: Applications to wing aerodynamic optimizations

Published:2016-10 Issue:5 Volume:29 Page:1178-1195
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

Şugar Gabor Oliviu,Koreanschi Andreea,Botez Ruxandra Mihaela

Funder

Natural Sciences and Engineering Research Council of Canada

CRIAQ MDO-505 project

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference51 articles.

1. International Civil Aviation Organisation (ICAO). Aviation’s contribution to climate change. Environmental Report; 2010. Available from: http://www.icao.int/.

2. Shape morphing of aircraft wings: Status and challenges;Sofla;Mater Des,2010

3. Adaptive wing and flow control technology;Stanewsky;Progr Aerospace Sci,2001

4. A review of morphing aircraft;Barbarino;J Intell Mater Syst Struct,2011

5. Gamboa P, Alexio P, Vale J, Lau F, Suleman A. Design and testing of a morphing wing for an experimental UAV. Neuilly-sur-Seine, France; 2007. Report No.: RTO-MP-AVT-146.

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