Design, aerodynamic analysis and optimization of a next‑generation commercial airliner (2022)
- Authors:
- USP affiliated authors: CATALANO, FERNANDO MARTINI - EESC ; MUÑOZ, HERNAN DARIO CERON - EESC ; MOSQUERA, PEDRO DAVID BRAVO - EESC
- Unidade: EESC
- DOI: 10.1007/s40430-022-03924-x
- Subjects: AERODINÂMICA DE AERONAVES; ENGENHARIA AERONÁUTICA
- Agências de fomento:
- Language: Inglês
- Imprenta:
- Publisher: Springer
- Publisher place: Heidelberg, Germany
- Date published: 2022
- Source:
- Título: Journal of the Brazilian Society of Mechanical Sciences and Engineering
- ISSN: 1678-5878
- Volume/Número/Paginação/Ano: v. 44, Article number 609, p. 1-22, 2022
- Este periódico é de assinatura
- Este artigo NÃO é de acesso aberto
- Cor do Acesso Aberto: closed
-
ABNT
BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Design, aerodynamic analysis and optimization of a next‑generation commercial airliner. Journal of the Brazilian Society of Mechanical Sciences and Engineering, v. 44, p. 1-22, 2022Tradução . . Disponível em: https://doi.org/10.1007/s40430-022-03924-x. Acesso em: 28 abr. 2025. -
APA
Bravo Mosquera, P. D., Cerón Muñoz, H. D., & Catalano, F. M. (2022). Design, aerodynamic analysis and optimization of a next‑generation commercial airliner. Journal of the Brazilian Society of Mechanical Sciences and Engineering, 44, 1-22. doi:10.1007/s40430-022-03924-x -
NLM
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design, aerodynamic analysis and optimization of a next‑generation commercial airliner [Internet]. Journal of the Brazilian Society of Mechanical Sciences and Engineering. 2022 ; 44 1-22.[citado 2025 abr. 28 ] Available from: https://doi.org/10.1007/s40430-022-03924-x -
Vancouver
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design, aerodynamic analysis and optimization of a next‑generation commercial airliner [Internet]. Journal of the Brazilian Society of Mechanical Sciences and Engineering. 2022 ; 44 1-22.[citado 2025 abr. 28 ] Available from: https://doi.org/10.1007/s40430-022-03924-x - Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system
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Informações sobre o DOI: 10.1007/s40430-022-03924-x (Fonte: oaDOI API)
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