Subjects: DINÂMICA DOS FLUÍDOS COMPUTACIONAL, TÚNEIS DE VENTO, AERODINÂMICA DE AERONAVES, PROJETO DE AERONAVES
ABNT
MOSQUERA, Pedro David Bravo. Methodologies for designing, optimizing, and evaluating possible unconventional aircraft configurations for future civil aviation. 2022. Tese (Doutorado) – Universidade de São Paulo, São Carlos, 2022. Disponível em: https://www.teses.usp.br/teses/disponiveis/18/18148/tde-19122022-155409/. Acesso em: 08 maio 2024.APA
Mosquera, P. D. B. (2022). Methodologies for designing, optimizing, and evaluating possible unconventional aircraft configurations for future civil aviation (Tese (Doutorado). Universidade de São Paulo, São Carlos. Recuperado de https://www.teses.usp.br/teses/disponiveis/18/18148/tde-19122022-155409/NLM
Mosquera PDB. Methodologies for designing, optimizing, and evaluating possible unconventional aircraft configurations for future civil aviation [Internet]. 2022 ;[citado 2024 maio 08 ] Available from: https://www.teses.usp.br/teses/disponiveis/18/18148/tde-19122022-155409/Vancouver
Mosquera PDB. Methodologies for designing, optimizing, and evaluating possible unconventional aircraft configurations for future civil aviation [Internet]. 2022 ;[citado 2024 maio 08 ] Available from: https://www.teses.usp.br/teses/disponiveis/18/18148/tde-19122022-155409/