Modeling of structural deflections on a F/A-18 aircraft following flight flutter tests by use of subspace identification method

De Jesus Mota, S., Nadeau-Beaulieu, M., Botez, Ruxandra and Brenner, M.. 2007. « Modeling of structural deflections on a F/A-18 aircraft following flight flutter tests by use of subspace identification method ». In AIAA Atmospheric Flight Mechanics Conference and Exhibit (Hilton Head, SC, USA, Aug. 20-23, 2007) Coll. « AIAA paper » pp. 42-53. Reston, VA, USA : American Institute of Aeronautics and Astronautics Inc..
Compte des citations dans Scopus : 4.

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Item Type:	Conference proceeding
ISBN:	9781563479052
Additional Information:	Identifiant de l'article: AIAA 2007-6303
Professor:	Professor Botez, Ruxandra
Affiliation:	Génie de la production automatisée
Date Deposited:	30 Oct 2012 18:17
Last Modified:	30 Oct 2012 18:17
URI:	https://espace2.etsmtl.ca/id/eprint/2536

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