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Artigo de periodico
Slat aerodynamic noise reduction using dielectric barrier discharge plasma actuators (2020)
Silva, Gabriel Pereira Gouveia da; Eguea, João Paulo; Croce, José Antonio Garcia; Catalano, Fernando Martini
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, FUSELAGEM DE AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
SILVA, Gabriel Pereira Gouveia da et al. Slat aerodynamic noise reduction using dielectric barrier discharge plasma actuators. Aerospace Science and Technology, v. 97, p. 1-11, 2020Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2019.105642. Acesso em: 28 set. 2024.
APA
Silva, G. P. G. da, Eguea, J. P., Croce, J. A. G., & Catalano, F. M. (2020). Slat aerodynamic noise reduction using dielectric barrier discharge plasma actuators. Aerospace Science and Technology, 97, 1-11. doi:10.1016/j.ast.2019.105642
NLM
Silva GPG da, Eguea JP, Croce JAG, Catalano FM. Slat aerodynamic noise reduction using dielectric barrier discharge plasma actuators [Internet]. Aerospace Science and Technology. 2020 ; 97 1-11.[citado 2024 set. 28 ] Available from: https://doi.org/10.1016/j.ast.2019.105642
Vancouver
Silva GPG da, Eguea JP, Croce JAG, Catalano FM. Slat aerodynamic noise reduction using dielectric barrier discharge plasma actuators [Internet]. Aerospace Science and Technology. 2020 ; 97 1-11.[citado 2024 set. 28 ] Available from: https://doi.org/10.1016/j.ast.2019.105642
Artigo de periodico
Fuel efficiency improvement on a business jet using a camber morphing winglet concept (2020)
Eguea, João Paulo; Silva, Gabriel Pereira Gouveia da; Catalano, Fernando Martini
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, COMBUSTÍVEIS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
EGUEA, João Paulo e SILVA, Gabriel Pereira Gouveia da e CATALANO, Fernando Martini. Fuel efficiency improvement on a business jet using a camber morphing winglet concept. Aerospace Science and Technology, v. 96, p. 1-9, 2020Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2019.105542. Acesso em: 28 set. 2024.
APA
Eguea, J. P., Silva, G. P. G. da, & Catalano, F. M. (2020). Fuel efficiency improvement on a business jet using a camber morphing winglet concept. Aerospace Science and Technology, 96, 1-9. doi:10.1016/j.ast.2019.105542
NLM
Eguea JP, Silva GPG da, Catalano FM. Fuel efficiency improvement on a business jet using a camber morphing winglet concept [Internet]. Aerospace Science and Technology. 2020 ; 96 1-9.[citado 2024 set. 28 ] Available from: https://doi.org/10.1016/j.ast.2019.105542
Vancouver
Eguea JP, Silva GPG da, Catalano FM. Fuel efficiency improvement on a business jet using a camber morphing winglet concept [Internet]. Aerospace Science and Technology. 2020 ; 96 1-9.[citado 2024 set. 28 ] Available from: https://doi.org/10.1016/j.ast.2019.105542
Artigo de periodico
Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraf (2019)
Bravo Mosquera, Pedro David; Abdalla, Alvaro Martins ; Cerón Muñoz, Hernán Darío ; Catalano, Fernando Martini
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: PROJETO DE AERONAVES, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BRAVO MOSQUERA, Pedro David et al. Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraf. Aerospace Science and Technology, v. 86, p. 497-519, 2019Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2019.01.059. Acesso em: 28 set. 2024.
APA
Bravo Mosquera, P. D., Abdalla, A. M., Cerón Muñoz, H. D., & Catalano, F. M. (2019). Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraf. Aerospace Science and Technology, 86, 497-519. doi:10.1016/j.ast.2019.01.059
NLM
Bravo Mosquera PD, Abdalla AM, Cerón Muñoz HD, Catalano FM. Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraf [Internet]. Aerospace Science and Technology. 2019 ; 86 497-519.[citado 2024 set. 28 ] Available from: https://doi.org/10.1016/j.ast.2019.01.059
Vancouver
Bravo Mosquera PD, Abdalla AM, Cerón Muñoz HD, Catalano FM. Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraf [Internet]. Aerospace Science and Technology. 2019 ; 86 497-519.[citado 2024 set. 28 ] Available from: https://doi.org/10.1016/j.ast.2019.01.059
Artigo de periodico
Conceptual design and CFD analysis of a new prototype of agricultural aircraft (2018)
Bravo Mosquera, Pedro David; Cerón Muñoz, Hernán Darío ; Díaz Vázquez, Guillermo; Catalano, Fernando Martini
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, AERONAVES AGRÍCOLAS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BRAVO MOSQUERA, Pedro David et al. Conceptual design and CFD analysis of a new prototype of agricultural aircraft. Aerospace Science and Technology, v. 80, p. 156-176, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2018.07.014. Acesso em: 28 set. 2024.
APA
Bravo Mosquera, P. D., Cerón Muñoz, H. D., Díaz Vázquez, G., & Catalano, F. M. (2018). Conceptual design and CFD analysis of a new prototype of agricultural aircraft. Aerospace Science and Technology, 80, 156-176. doi:10.1016/j.ast.2018.07.014
NLM
Bravo Mosquera PD, Cerón Muñoz HD, Díaz Vázquez G, Catalano FM. Conceptual design and CFD analysis of a new prototype of agricultural aircraft [Internet]. Aerospace Science and Technology. 2018 ; 80 156-176.[citado 2024 set. 28 ] Available from: https://doi.org/10.1016/j.ast.2018.07.014
Vancouver
Bravo Mosquera PD, Cerón Muñoz HD, Díaz Vázquez G, Catalano FM. Conceptual design and CFD analysis of a new prototype of agricultural aircraft [Internet]. Aerospace Science and Technology. 2018 ; 80 156-176.[citado 2024 set. 28 ] Available from: https://doi.org/10.1016/j.ast.2018.07.014
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
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: 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: 28 set. 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 set. 28 ] 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 set. 28 ] Available from: https://doi.org/10.1016/j.ast.2017.09.005

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