Segui, Marine, Mantilla, Matthieu et Botez, Ruxandra.
2 October 2018.
« Original Methods for Finding a Wing Shape Airfoil ».
[Research article]. Substance ÉTS.
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Official URL: https://substance.etsmtl.ca/en/methodes-originales...
Abstract
In view of the future application of a morphing wing technology on the horizontal tail of the Cessna Citation X, the LARCASE team had to develop an accurate aerodynamic model of the horizontal tail. To this end, a geometry of the wing was required, especially its airfoil shape, which is strictly confidential. Using a reverse engineering method, the team managed to find an airfoil that delivered a performance close to the original one.
Item Type: | Non-peer reviewed article published in a journal or magazine | ||
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Refereed: | No | ||
Uncontrolled Keywords: | Airfoil, Morphing, Horizontal Tail, Optimization, Performance, Parameterization, Bezier-Parsec, Particle Swarm Algorithm, Aerodynamic, Cessna Citation X | ||
Professor: |
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Affiliation: | Génie de la production automatisée | ||
Date Deposited: | 26 Mar 2019 16:04 | ||
Last Modified: | 19 Sep 2019 20:20 | ||
URI: | https://espace2.etsmtl.ca/id/eprint/18338 |
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