Original Methods for Finding a Wing Shape Airfoil

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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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
Refereed:	No
Uncontrolled Keywords:	Airfoil, Morphing, Horizontal Tail, Optimization, Performance, Parameterization, Bezier-Parsec, Particle Swarm Algorithm, Aerodynamic, Cessna Citation X
Professor:	Professor Botez, Ruxandra
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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