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Wing component allocation for a morphing variable span of tapered wing using finite element method and topology optimisation - Application to the UAS-S4

Elelwi, M., Calvet, T., Botez, R. M. et Dao, T. M.. 2021. « Wing component allocation for a morphing variable span of tapered wing using finite element method and topology optimisation - Application to the UAS-S4 ». Aeronautical Journal, vol. 125, nº 1290. pp. 1313-1336.

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Item Type: Peer reviewed article published in a journal
Professor:
Professor
Botez, Ruxandra
Dao, Thien-My
Affiliation: Génie des systèmes, Génie mécanique
Date Deposited: 28 Jul 2021 20:44
Last Modified: 01 Sep 2021 19:38
URI: https://espace2.etsmtl.ca/id/eprint/22912

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