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Artigo de periodico
Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study (2023)
Bravo Mosquera, Pedro David; Cerón Muñoz, Hernán Darío ; Catalano, Fernando Martini
Fonte: Aerospace. Unidade: EESC
Assuntos: AERODINÂMICA DE AERONAVES, TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study. Aerospace, v. 10, n. 7, p. 1-26, 2023Tradução . . Disponível em: https://doi.org/10.3390/aerospace10070651. Acesso em: 18 out. 2024.
APA
Bravo Mosquera, P. D., Cerón Muñoz, H. D., & Catalano, F. M. (2023). Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study. Aerospace, 10( 7), 1-26. doi:10.3390/aerospace10070651
NLM
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study [Internet]. Aerospace. 2023 ; 10( 7): 1-26.[citado 2024 out. 18 ] Available from: https://doi.org/10.3390/aerospace10070651
Vancouver
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study [Internet]. Aerospace. 2023 ; 10( 7): 1-26.[citado 2024 out. 18 ] Available from: https://doi.org/10.3390/aerospace10070651
Tese (Doutorado)
Methodologies for designing, optimizing, and evaluating possible unconventional aircraft configurations for future civil aviation (2022)
Mosquera, Pedro David Bravo; Catalano, Fernando Martini (Orientador)
Unidade: EESC
Assuntos: DINÂMICA DOS FLUÍDOS COMPUTACIONAL, TÚNEIS DE VENTO, AERODINÂMICA DE AERONAVES, PROJETO DE AERONAVES
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 18 out. 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 out. 18 ] 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 out. 18 ] Available from: https://www.teses.usp.br/teses/disponiveis/18/18148/tde-19122022-155409/
Artigo de periodico
Aerodynamic design analysis of a UAV for superficial research of volcanic environments (2017)
Bravo Mosquera, Pedro David; Botero Bolívar, Laura; Acevedo Giraldo, Daniel; Cerón Muñoz, Hernán Darío
Fonte: Aerospace Science and Technology. Unidade: EESC
Assuntos: AERODINÂMICA DE AERONAVES, TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BRAVO MOSQUERA, Pedro David et al. Aerodynamic design analysis of a UAV for superficial research of volcanic environments. Aerospace Science and Technology, v. 70, p. 600-614, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2017.09.005. Acesso em: 18 out. 2024.
APA
Bravo Mosquera, P. D., Botero Bolívar, L., Acevedo Giraldo, D., & Cerón Muñoz, H. D. (2017). Aerodynamic design analysis of a UAV for superficial research of volcanic environments. Aerospace Science and Technology, 70, 600-614. doi:10.1016/j.ast.2017.09.005
NLM
Bravo Mosquera PD, Botero Bolívar L, Acevedo Giraldo D, Cerón Muñoz HD. Aerodynamic design analysis of a UAV for superficial research of volcanic environments [Internet]. Aerospace Science and Technology. 2017 ; 70 600-614.[citado 2024 out. 18 ] Available from: https://doi.org/10.1016/j.ast.2017.09.005
Vancouver
Bravo Mosquera PD, Botero Bolívar L, Acevedo Giraldo D, Cerón Muñoz HD. Aerodynamic design analysis of a UAV for superficial research of volcanic environments [Internet]. Aerospace Science and Technology. 2017 ; 70 600-614.[citado 2024 out. 18 ] Available from: https://doi.org/10.1016/j.ast.2017.09.005
Trabalho de evento
Experimental assessment of a low reynolds number vehicle (2017)
Acevedo Giraldo, Daniel; Botero Bolívar, Laura; Bravo Mosquera, Pedro David; Cerón Muñoz, Hernán Darío ; Catalano, Fernando Martini
Fonte: Anais. Nome do evento: International Congress of Mechanical Engineering - COBEM. Unidade: EESC
Assuntos: AEROFÓLIOS, TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
ACEVEDO GIRALDO, Daniel et al. Experimental assessment of a low reynolds number vehicle. 2017, Anais.. Rio de Janeiro, RJ: ABCM, 2017. Disponível em: https://repositorio.usp.br/directbitstream/8edff6fb-cef9-4db0-8759-0d18d987db28/trabalho%2017%20-%20EXPERIMENTAL%20ASSESMENT%20OF%20A%20LOW%20REYNOLDS%20NUMBER%20VEHICLE%20%28COBEM%202017%29.pdf. Acesso em: 18 out. 2024.
APA
Acevedo Giraldo, D., Botero Bolívar, L., Bravo Mosquera, P. D., Cerón Muñoz, H. D., & Catalano, F. M. (2017). Experimental assessment of a low reynolds number vehicle. In Anais. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/8edff6fb-cef9-4db0-8759-0d18d987db28/trabalho%2017%20-%20EXPERIMENTAL%20ASSESMENT%20OF%20A%20LOW%20REYNOLDS%20NUMBER%20VEHICLE%20%28COBEM%202017%29.pdf
NLM
Acevedo Giraldo D, Botero Bolívar L, Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Experimental assessment of a low reynolds number vehicle [Internet]. Anais. 2017 ;[citado 2024 out. 18 ] Available from: https://repositorio.usp.br/directbitstream/8edff6fb-cef9-4db0-8759-0d18d987db28/trabalho%2017%20-%20EXPERIMENTAL%20ASSESMENT%20OF%20A%20LOW%20REYNOLDS%20NUMBER%20VEHICLE%20%28COBEM%202017%29.pdf
Vancouver
Acevedo Giraldo D, Botero Bolívar L, Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Experimental assessment of a low reynolds number vehicle [Internet]. Anais. 2017 ;[citado 2024 out. 18 ] Available from: https://repositorio.usp.br/directbitstream/8edff6fb-cef9-4db0-8759-0d18d987db28/trabalho%2017%20-%20EXPERIMENTAL%20ASSESMENT%20OF%20A%20LOW%20REYNOLDS%20NUMBER%20VEHICLE%20%28COBEM%202017%29.pdf

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