Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Michelle F. Westin"'
Autor:
Michelle F. Westin, Jose M. Balthazar, Roberto G. A. da Silva, Mauricio A. Ribeiro, Angelo M. Tusset
Publikováno v:
Axioms, Vol 12, Iss 9, p 826 (2023)
The objective of this article is to characterize an aeroelastic system in terms of its dynamical behavior, which could be either chaotic or periodic before, during, and after achieving the flutter velocity. The aeroelastic system shown here is a wing
Externí odkaz:
https://doaj.org/article/77225091e1064399a6a638f303b4ecd9
Autor:
Maria Coutinho, David Bento, Alain Souza, Rodrigo Cruz, Frederico Afonso, Fernando Lau, Afzal Suleman, Felipe R. Barbosa, Ricardo Gandolfi, Walter Affonso, Felipe I.K. Odaguil, Michelle F. Westin, Ricardo J.N. dos Reis, Carlos R.I. da Silva
Publikováno v:
Applied Thermal Engineering. 227:120427
The electrification of aircraft propulsive systems has been identified as one of the potential solutions towards a lower carbon footprint in the aviation industry. However, there are still several environmental and technological challenges associated
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::51a89c07cc58fbf0d8558e263754dc12
https://doi.org/10.1016/j.applthermaleng.2023.120427
https://doi.org/10.1016/j.applthermaleng.2023.120427
Publikováno v:
Bowen, L L, Celik, A, Azarpeyvand, M & Westin, M F 2022, The effect of angle of attack on turbulence interaction noise with a porous leading edge . in 28th AIAA/CEAS Aeroacoustics Conference, 2022 : Session: Acoustic/Fluid Dynamics Interactions IX: Misc ., AIAA 2022-3095, 28th AIAA/CEAS Aeroacoustics Conference, 2022, American Institute of Aeronautics and Astronautics Inc. (AIAA), 28th AIAA/CEAS Aeroacoustics 2022 Conference, Southampton, United Kingdom, 14/06/22 . https://doi.org/10.2514/6.2022-3095
The paper is concerned with the effect of angle of attack on the interaction noise between a turbulent flow and a NACA 0012 airfoil. This experimental study considers an airfoil with a porous leading edge up to 10% of the chord and compares the noise
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9ebb4e680134786703a8df65e71e4a8c
https://doi.org/10.2514/6.2022-3095
https://doi.org/10.2514/6.2022-3095
Publikováno v:
Journal of Vibration Engineering & Technologies. 9:303-312
This paper aims to investigate the post-flutter nonlinearities due to the wing high aspect ratio. Flutter is an aerodynamic auto-excited phenomenon which occurs due to the coupling of two or more different vibration modes. This coupling results from
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f8c1d86a16ba9268b4d85727a6921efe
https://doi.org/10.1007/s42417-020-00227-0
https://doi.org/10.1007/s42417-020-00227-0
Autor:
Airton Nabarrete, Angelo Marcelo Tusset, José Manoel Balthazar, Roberto Gil Annes da Silva, Michelle F. Westin, Guênia Mara Vieira Ladeira
Publikováno v:
Procceedings of the 24th ABCM International Congress of Mechanicl Engineering.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a8abab8139a79845450188e9f0f19522
https://doi.org/10.26678/abcm.cobem2017.cob17-0201
https://doi.org/10.26678/abcm.cobem2017.cob17-0201
Autor:
Michelle F. Westin, José Manoel Balthazar, Roberto Gil Annes da Silva, Mateus de Freitas Virgílio Pereira, Airton Nabarrete
Publikováno v:
AIAA Modeling and Simulation Technologies Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6314158b5d0eff2232ed184b01b69115
https://doi.org/10.2514/6.2016-3834
https://doi.org/10.2514/6.2016-3834