Segui, Marine, Mantilla, Matthieu et Botez, Ruxandra.
2 octobre 2018.
« Original Methods for Finding a Wing Shape Airfoil ».
[Article de recherche]. Substance ÉTS.
Prévisualisation |
PDF
Substance 2018 18338 Original Methods for Finding a Wing Shape Airfoil - Substance.pdf Télécharger (1MB) | Prévisualisation |
URL Officielle: https://substance.etsmtl.ca/en/methodes-originales...
Résumé
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.
| Type de document: | Article de revue ou de magazine, non révisé par les pairs |
|---|---|
| Validation par les pairs: | Non |
| Mots-clés libres: | Airfoil, Morphing, Horizontal Tail, Optimization, Performance, Parameterization, Bezier-Parsec, Particle Swarm Algorithm, Aerodynamic, Cessna Citation X |
| Professeur: | Professeur Botez, Ruxandra |
| Affiliation: | Génie de la production automatisée |
| Date de dépôt: | 26 mars 2019 16:04 |
| Dernière modification: | 19 sept. 2019 20:20 |
| URI: | https://espace2.etsmtl.ca/id/eprint/18338 |
Actions (Authentification requise)
 |
Dernière vérification avant le dépôt |