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Artigo de periodico
Experimental analysis of bio-inspired vortex generators on a blade with S822 airfoil (2023)
Parra, Hector G.; Cerón Muñoz, Hernán Darío ; Gomez, William; Gaona, Elvis E.
Source: Energies. Unidade: EESC
Subjects: TURBINAS, VIBRAÇÕES DE AERONAVES, TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA
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ABNT
PARRA, Hector G. et al. Experimental analysis of bio-inspired vortex generators on a blade with S822 airfoil. Energies, v. 16, n. 12, p. 1-22, 2023Tradução . . Disponível em: https://doi.org/10.3390/en16124538. Acesso em: 30 set. 2024.
APA
Parra, H. G., Cerón Muñoz, H. D., Gomez, W., & Gaona, E. E. (2023). Experimental analysis of bio-inspired vortex generators on a blade with S822 airfoil. Energies, 16( 12), 1-22. doi:10.3390/en16124538
NLM
Parra HG, Cerón Muñoz HD, Gomez W, Gaona EE. Experimental analysis of bio-inspired vortex generators on a blade with S822 airfoil [Internet]. Energies. 2023 ; 16( 12): 1-22.[citado 2024 set. 30 ] Available from: https://doi.org/10.3390/en16124538
Vancouver
Parra HG, Cerón Muñoz HD, Gomez W, Gaona EE. Experimental analysis of bio-inspired vortex generators on a blade with S822 airfoil [Internet]. Energies. 2023 ; 16( 12): 1-22.[citado 2024 set. 30 ] Available from: https://doi.org/10.3390/en16124538
Trabalho de evento-resumo
A study of the aerodynamic behavior of a hypersonic waverider vehicle by means of CFD (2023)
Guzmán-Bohórquez, Rolando; Cerón Muñoz, Hernán Darío ; Greco Júnior, Paulo Celso
Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC
Assunto: AERODINÂMICA
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ABNT
GUZMÁN-BOHÓRQUEZ, Rolando e CERÓN MUÑOZ, Hernán Darío e GRECO JÚNIOR, Paulo Celso. A study of the aerodynamic behavior of a hypersonic waverider vehicle by means of CFD. 2023, Anais.. São Carlos, SP: EESC-USP, 2023. Disponível em: http://soac.eesc.usp.br/index.php/SiPGEM/viisipgem/paper/view/3814/2645. Acesso em: 30 set. 2024.
APA
Guzmán-Bohórquez, R., Cerón Muñoz, H. D., & Greco Júnior, P. C. (2023). A study of the aerodynamic behavior of a hypersonic waverider vehicle by means of CFD. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/SiPGEM/viisipgem/paper/view/3814/2645
NLM
Guzmán-Bohórquez R, Cerón Muñoz HD, Greco Júnior PC. A study of the aerodynamic behavior of a hypersonic waverider vehicle by means of CFD [Internet]. Anais. 2023 ;[citado 2024 set. 30 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/viisipgem/paper/view/3814/2645
Vancouver
Guzmán-Bohórquez R, Cerón Muñoz HD, Greco Júnior PC. A study of the aerodynamic behavior of a hypersonic waverider vehicle by means of CFD [Internet]. Anais. 2023 ;[citado 2024 set. 30 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/viisipgem/paper/view/3814/2645
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
Source: Aerospace. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA
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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: 30 set. 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 set. 30 ] 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 set. 30 ] Available from: https://doi.org/10.3390/aerospace10070651
Trabalho de evento-resumo
Aerodynamics analysis of three-dimensional bump in high-speed supersonic flow (2023)
Vaca Rios, John Jairo; Cerón Muñoz, Hernán Darío
Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC
Subjects: COLISÕES, DINÂMICA DOS FLUÍDOS
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ABNT
VACA RIOS, John Jairo e CERÓN MUÑOZ, Hernán Darío. Aerodynamics analysis of three-dimensional bump in high-speed supersonic flow. 2023, Anais.. São Carlos, SP: EESC-USP, 2023. Disponível em: http://soac.eesc.usp.br/index.php/SiPGEM/viisipgem/paper/view/3804/2648. Acesso em: 30 set. 2024.
APA
Vaca Rios, J. J., & Cerón Muñoz, H. D. (2023). Aerodynamics analysis of three-dimensional bump in high-speed supersonic flow. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/SiPGEM/viisipgem/paper/view/3804/2648
NLM
Vaca Rios JJ, Cerón Muñoz HD. Aerodynamics analysis of three-dimensional bump in high-speed supersonic flow [Internet]. Anais. 2023 ;[citado 2024 set. 30 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/viisipgem/paper/view/3804/2648
Vancouver
Vaca Rios JJ, Cerón Muñoz HD. Aerodynamics analysis of three-dimensional bump in high-speed supersonic flow [Internet]. Anais. 2023 ;[citado 2024 set. 30 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/viisipgem/paper/view/3804/2648
Artigo de periodico
Experimental analysis of oscillatory vortex generators in wind turbine blade (2023)
Parra, Hector G.; Cerón Muñoz, Hernán Darío ; Gomez, William; Gaona, Elvis E.
Source: Energies. Unidade: EESC
Subjects: TÚNEIS DE VENTO, TURBINAS, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
PARRA, Hector G. et al. Experimental analysis of oscillatory vortex generators in wind turbine blade. Energies, v. 16, n. 11, p. 1-14, 2023Tradução . . Disponível em: https://doi.org/10.3390/en16114343. Acesso em: 30 set. 2024.
APA
Parra, H. G., Cerón Muñoz, H. D., Gomez, W., & Gaona, E. E. (2023). Experimental analysis of oscillatory vortex generators in wind turbine blade. Energies, 16( 11), 1-14. doi:10.3390/en16114343
NLM
Parra HG, Cerón Muñoz HD, Gomez W, Gaona EE. Experimental analysis of oscillatory vortex generators in wind turbine blade [Internet]. Energies. 2023 ; 16( 11): 1-14.[citado 2024 set. 30 ] Available from: https://doi.org/10.3390/en16114343
Vancouver
Parra HG, Cerón Muñoz HD, Gomez W, Gaona EE. Experimental analysis of oscillatory vortex generators in wind turbine blade [Internet]. Energies. 2023 ; 16( 11): 1-14.[citado 2024 set. 30 ] Available from: https://doi.org/10.3390/en16114343
Artigo de periodico
Design, aerodynamic analysis and optimization of a next‑generation commercial airliner (2022)
Bravo Mosquera, Pedro David; Cerón Muñoz, Hernán Darío ; Catalano, Fernando Martini
Source: Journal of the Brazilian Society of Mechanical Sciences and Engineering. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
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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: 30 set. 2024.
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 2024 set. 30 ] 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 2024 set. 30 ] Available from: https://doi.org/10.1007/s40430-022-03924-x
Trabalho de evento-resumo
Efeitos aeroacústicos do bordo de ataque serrilhado (WLE) no estator SDT de uma bancada "RIG-FAN" (2022)
Garcia, Andressa Caroline Rodrigues; Cerón Muñoz, Hernán Darío
Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC
Subjects: AEROACÚSTICA, ENGENHARIA MECÂNICA
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ABNT
GARCIA, Andressa Caroline Rodrigues e CERÓN MUÑOZ, Hernán Darío. Efeitos aeroacústicos do bordo de ataque serrilhado (WLE) no estator SDT de uma bancada "RIG-FAN". 2022, Anais.. São Carlos, SP: EESC-USP, 2022. Disponível em: http://soac.eesc.usp.br/index.php/SiPGEM/visipgem/paper/view/3485/2555. Acesso em: 30 set. 2024.
APA
Garcia, A. C. R., & Cerón Muñoz, H. D. (2022). Efeitos aeroacústicos do bordo de ataque serrilhado (WLE) no estator SDT de uma bancada "RIG-FAN". In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/SiPGEM/visipgem/paper/view/3485/2555
NLM
Garcia ACR, Cerón Muñoz HD. Efeitos aeroacústicos do bordo de ataque serrilhado (WLE) no estator SDT de uma bancada "RIG-FAN" [Internet]. Anais. 2022 ;[citado 2024 set. 30 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/visipgem/paper/view/3485/2555
Vancouver
Garcia ACR, Cerón Muñoz HD. Efeitos aeroacústicos do bordo de ataque serrilhado (WLE) no estator SDT de uma bancada "RIG-FAN" [Internet]. Anais. 2022 ;[citado 2024 set. 30 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/visipgem/paper/view/3485/2555
Artigo de periodico-carta/editorial
Editorial (2020)
Pozo, Francesc; Tibaduiza, Diego A.; Torres-Arredondo, Miguel Ángel; Varón, Margarita; Cerón Muñoz, Hernán Darío
Source: International Journal of Distributed Sensor Networks. Unidade: EESC
Subjects: INTEGRIDADE ESTRUTURAL, ENSAIOS NÃO DESTRUTIVOS, AERONÁUTICA
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ABNT
POZO, Francesc et al. Editorial. International Journal of Distributed Sensor Networks. Thousand Oaks, CA, USA: Escola de Engenharia de São Carlos, Universidade de São Paulo. Disponível em: https://doi.org/10.1177/1550147720963270. Acesso em: 30 set. 2024. , 2020
APA
Pozo, F., Tibaduiza, D. A., Torres-Arredondo, M. Á., Varón, M., & Cerón Muñoz, H. D. (2020). Editorial. International Journal of Distributed Sensor Networks. Thousand Oaks, CA, USA: Escola de Engenharia de São Carlos, Universidade de São Paulo. doi:10.1177/1550147720963270
NLM
Pozo F, Tibaduiza DA, Torres-Arredondo MÁ, Varón M, Cerón Muñoz HD. Editorial [Internet]. International Journal of Distributed Sensor Networks. 2020 ; 16( 9): 1-2.[citado 2024 set. 30 ] Available from: https://doi.org/10.1177/1550147720963270
Vancouver
Pozo F, Tibaduiza DA, Torres-Arredondo MÁ, Varón M, Cerón Muñoz HD. Editorial [Internet]. International Journal of Distributed Sensor Networks. 2020 ; 16( 9): 1-2.[citado 2024 set. 30 ] Available from: https://doi.org/10.1177/1550147720963270
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
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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: 30 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. 30 ] 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. 30 ] Available from: https://doi.org/10.1016/j.ast.2019.01.059
Trabalho de evento
Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system (2019)
Bravo Mosquera, Pedro David; Cerón Muñoz, Hernán Darío ; Catalano, Fernando Martini
Source: Proceedings. Conference titles: AIAA Propulsion and Energy Forum. Unidade: EESC
Subjects: ENGENHARIA AERONÁUTICA, ASAS DE AERONAVES, AERODINÂMICA DE AERONAVES
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ABNT
BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-3850. Acesso em: 30 set. 2024.
APA
Bravo Mosquera, P. D., Cerón Muñoz, H. D., & Catalano, F. M. (2019). Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-3850
NLM
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system [Internet]. Proceedings. 2019 ;[citado 2024 set. 30 ] Available from: https://doi.org/10.2514/6.2019-3850
Vancouver
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system [Internet]. Proceedings. 2019 ;[citado 2024 set. 30 ] Available from: https://doi.org/10.2514/6.2019-3850
Trabalho de evento
Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application (2019)
Ribeiro, Daniel Garcia; Bravo Mosquera, Pedro David; Cerón Muñoz, Hernán Darío
Source: Proceedings. Conference titles: AIAA Propulsion and Energy Forum. Unidade: EESC
Subjects: TRANSFERÊNCIA DE CALOR, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
RIBEIRO, Daniel Garcia e BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío. Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://repositorio.usp.br/directbitstream/558bdbaf-a0df-406a-aee5-d60273db8fa1/trabalho%2001%20-%20Heat%20transfer%20effects%20on%20aerodynamic%20performance%20of%20a%20S809%20airfoil%20for%20wind%20turbine%20application%20%28AIAA%20Propulsion%20and%20Energy%202019%20Forum%29.pdf. Acesso em: 30 set. 2024.
APA
Ribeiro, D. G., Bravo Mosquera, P. D., & Cerón Muñoz, H. D. (2019). Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/558bdbaf-a0df-406a-aee5-d60273db8fa1/trabalho%2001%20-%20Heat%20transfer%20effects%20on%20aerodynamic%20performance%20of%20a%20S809%20airfoil%20for%20wind%20turbine%20application%20%28AIAA%20Propulsion%20and%20Energy%202019%20Forum%29.pdf
NLM
Ribeiro DG, Bravo Mosquera PD, Cerón Muñoz HD. Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application [Internet]. Proceedings. 2019 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/558bdbaf-a0df-406a-aee5-d60273db8fa1/trabalho%2001%20-%20Heat%20transfer%20effects%20on%20aerodynamic%20performance%20of%20a%20S809%20airfoil%20for%20wind%20turbine%20application%20%28AIAA%20Propulsion%20and%20Energy%202019%20Forum%29.pdf
Vancouver
Ribeiro DG, Bravo Mosquera PD, Cerón Muñoz HD. Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application [Internet]. Proceedings. 2019 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/558bdbaf-a0df-406a-aee5-d60273db8fa1/trabalho%2001%20-%20Heat%20transfer%20effects%20on%20aerodynamic%20performance%20of%20a%20S809%20airfoil%20for%20wind%20turbine%20application%20%28AIAA%20Propulsion%20and%20Energy%202019%20Forum%29.pdf
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
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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: 30 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. 30 ] 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. 30 ] Available from: https://doi.org/10.1016/j.ast.2018.07.014
Trabalho de evento
Aerodynamic heating effect on roughness, aerodynamic coefficients and power output of aerogenerators: a discussion (2018)
Ribeiro, Daniel Garcia; Cerón Muñoz, Hernán Darío ; Bravo Mosquera, Pedro David
Source: Proceedings of ENCIT. Conference titles: Brazilian Congress of Thermal Sciences and Engineering. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, TURBINAS, ENGENHARIA AERONÁUTICA
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ABNT
RIBEIRO, Daniel Garcia e CERÓN MUÑOZ, Hernán Darío e BRAVO MOSQUERA, Pedro David. Aerodynamic heating effect on roughness, aerodynamic coefficients and power output of aerogenerators: a discussion. 2018, Anais.. Rio de Janeiro, RJ: ABCM, 2018. Disponível em: https://repositorio.usp.br/directbitstream/715b85dc-28f5-4e9a-b32f-eb96c4d45f34/trabalho%2006%20-%20Aerodynamic%20Heating%20Effect%20on%20Roughness%2C%20Aerodynamic%20Coefficients%20and%20Power%20Output%20of%20Aerogenerators%20-%20a%20Discussion%20%2817th%20Brazilian%20Congress%20of%20Thermal%20Sciences%20and%20Engineering%202018%29_removed.pdf. Acesso em: 30 set. 2024.
APA
Ribeiro, D. G., Cerón Muñoz, H. D., & Bravo Mosquera, P. D. (2018). Aerodynamic heating effect on roughness, aerodynamic coefficients and power output of aerogenerators: a discussion. In Proceedings of ENCIT. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/715b85dc-28f5-4e9a-b32f-eb96c4d45f34/trabalho%2006%20-%20Aerodynamic%20Heating%20Effect%20on%20Roughness%2C%20Aerodynamic%20Coefficients%20and%20Power%20Output%20of%20Aerogenerators%20-%20a%20Discussion%20%2817th%20Brazilian%20Congress%20of%20Thermal%20Sciences%20and%20Engineering%202018%29_removed.pdf
NLM
Ribeiro DG, Cerón Muñoz HD, Bravo Mosquera PD. Aerodynamic heating effect on roughness, aerodynamic coefficients and power output of aerogenerators: a discussion [Internet]. Proceedings of ENCIT. 2018 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/715b85dc-28f5-4e9a-b32f-eb96c4d45f34/trabalho%2006%20-%20Aerodynamic%20Heating%20Effect%20on%20Roughness%2C%20Aerodynamic%20Coefficients%20and%20Power%20Output%20of%20Aerogenerators%20-%20a%20Discussion%20%2817th%20Brazilian%20Congress%20of%20Thermal%20Sciences%20and%20Engineering%202018%29_removed.pdf
Vancouver
Ribeiro DG, Cerón Muñoz HD, Bravo Mosquera PD. Aerodynamic heating effect on roughness, aerodynamic coefficients and power output of aerogenerators: a discussion [Internet]. Proceedings of ENCIT. 2018 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/715b85dc-28f5-4e9a-b32f-eb96c4d45f34/trabalho%2006%20-%20Aerodynamic%20Heating%20Effect%20on%20Roughness%2C%20Aerodynamic%20Coefficients%20and%20Power%20Output%20of%20Aerogenerators%20-%20a%20Discussion%20%2817th%20Brazilian%20Congress%20of%20Thermal%20Sciences%20and%20Engineering%202018%29_removed.pdf
Trabalho de evento
Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica (2018)
Parra Peñuela, Héctor; Gómez Rivera, William; Cerón Muñoz, Hernán Darío
Source: Proceedings. Conference titles: Congreso Latinoamericano de Ingeniería Mecánica - COLIM. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, TURBINAS, ENERGIA EÓLICA, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
PARRA PEÑUELA, Héctor e GÓMEZ RIVERA, William e CERÓN MUÑOZ, Hernán Darío. Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica. 2018, Anais.. Pamplona, Colômbia: Universidad Pamplona, 2018. Disponível em: https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf. Acesso em: 30 set. 2024.
APA
Parra Peñuela, H., Gómez Rivera, W., & Cerón Muñoz, H. D. (2018). Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica. In Proceedings. Pamplona, Colômbia: Universidad Pamplona. Recuperado de https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf
NLM
Parra Peñuela H, Gómez Rivera W, Cerón Muñoz HD. Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica [Internet]. Proceedings. 2018 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf
Vancouver
Parra Peñuela H, Gómez Rivera W, Cerón Muñoz HD. Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica [Internet]. Proceedings. 2018 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf
Trabalho de evento
Comparación de herramientas de simulación CFD en el estudion del efecto vórtice sobre punta de aspa para rotor eólico (2018)
Ortegon Sarmiento, Tatiana; Gómez Rivera, William; Cerón Muñoz, Hernán Darío
Source: Proceedings. Conference titles: Congreso Latinoamericano de Ingeniería Mecánica - COLIM. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, DINÂMICA DOS FLUÍDOS, ENERGIA EÓLICA, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
ORTEGON SARMIENTO, Tatiana e GÓMEZ RIVERA, William e CERÓN MUÑOZ, Hernán Darío. Comparación de herramientas de simulación CFD en el estudion del efecto vórtice sobre punta de aspa para rotor eólico. 2018, Anais.. Pamplona, Colômbia: Universidad Pamplona, 2018. Disponível em: https://repositorio.usp.br/directbitstream/1256ebe2-a474-4f95-b89d-c41cb18c47d1/trabalho%2007%20-%20COMPARISON%20OF%20CFD%20SIMULATION%20TOOLS%20IN%20THE%20STUDY%20OF%20VORTEX%20EFFECT%20ON%20WIND%20ROTOR%20BLADE%20TIP%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29_removed.pdf. Acesso em: 30 set. 2024.
APA
Ortegon Sarmiento, T., Gómez Rivera, W., & Cerón Muñoz, H. D. (2018). Comparación de herramientas de simulación CFD en el estudion del efecto vórtice sobre punta de aspa para rotor eólico. In Proceedings. Pamplona, Colômbia: Universidad Pamplona. Recuperado de https://repositorio.usp.br/directbitstream/1256ebe2-a474-4f95-b89d-c41cb18c47d1/trabalho%2007%20-%20COMPARISON%20OF%20CFD%20SIMULATION%20TOOLS%20IN%20THE%20STUDY%20OF%20VORTEX%20EFFECT%20ON%20WIND%20ROTOR%20BLADE%20TIP%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29_removed.pdf
NLM
Ortegon Sarmiento T, Gómez Rivera W, Cerón Muñoz HD. Comparación de herramientas de simulación CFD en el estudion del efecto vórtice sobre punta de aspa para rotor eólico [Internet]. Proceedings. 2018 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/1256ebe2-a474-4f95-b89d-c41cb18c47d1/trabalho%2007%20-%20COMPARISON%20OF%20CFD%20SIMULATION%20TOOLS%20IN%20THE%20STUDY%20OF%20VORTEX%20EFFECT%20ON%20WIND%20ROTOR%20BLADE%20TIP%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29_removed.pdf
Vancouver
Ortegon Sarmiento T, Gómez Rivera W, Cerón Muñoz HD. Comparación de herramientas de simulación CFD en el estudion del efecto vórtice sobre punta de aspa para rotor eólico [Internet]. Proceedings. 2018 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/1256ebe2-a474-4f95-b89d-c41cb18c47d1/trabalho%2007%20-%20COMPARISON%20OF%20CFD%20SIMULATION%20TOOLS%20IN%20THE%20STUDY%20OF%20VORTEX%20EFFECT%20ON%20WIND%20ROTOR%20BLADE%20TIP%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29_removed.pdf
Artigo de periodico
Redesign of an experimental Unmanned Aerial Vehicle (UAV) for its conversion into an operational laboratory platform (2018)
White, Philippe; Vaca, John; Villalba, Jorge; Martinez, Diego; Pardo, Gerardo; Cerón Muñoz, Hernán Darío
Source: International Journal of Applied Enginering Research. Unidade: EESC
Subjects: AERONAVES NÃO TRIPULADAS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
WHITE, Philippe et al. Redesign of an experimental Unmanned Aerial Vehicle (UAV) for its conversion into an operational laboratory platform. International Journal of Applied Enginering Research, v. 13, n. 23, p. 16438-16446, 2018Tradução . . Disponível em: https://repositorio.usp.br/directbitstream/b4c197e2-f162-4d99-a5bc-8ea9e8b28e47/artigo%2003%20-%20Redesign%20of%20an%20experimental%20Unmanned%20Aerial%20Vehicle%20%28UAV%29%20for%20its%20conversion%20into%20an%20operational%20laboratory%20platform%20%28INTERNATIONAL%20JOURNAL%20OF%20APPLIED%20ENGINEERING%20RESEARCH%29.pdf. Acesso em: 30 set. 2024.
APA
White, P., Vaca, J., Villalba, J., Martinez, D., Pardo, G., & Cerón Muñoz, H. D. (2018). Redesign of an experimental Unmanned Aerial Vehicle (UAV) for its conversion into an operational laboratory platform. International Journal of Applied Enginering Research, 13( 23), 16438-16446. Recuperado de https://repositorio.usp.br/directbitstream/b4c197e2-f162-4d99-a5bc-8ea9e8b28e47/artigo%2003%20-%20Redesign%20of%20an%20experimental%20Unmanned%20Aerial%20Vehicle%20%28UAV%29%20for%20its%20conversion%20into%20an%20operational%20laboratory%20platform%20%28INTERNATIONAL%20JOURNAL%20OF%20APPLIED%20ENGINEERING%20RESEARCH%29.pdf
NLM
White P, Vaca J, Villalba J, Martinez D, Pardo G, Cerón Muñoz HD. Redesign of an experimental Unmanned Aerial Vehicle (UAV) for its conversion into an operational laboratory platform [Internet]. International Journal of Applied Enginering Research. 2018 ; 13( 23): 16438-16446.[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/b4c197e2-f162-4d99-a5bc-8ea9e8b28e47/artigo%2003%20-%20Redesign%20of%20an%20experimental%20Unmanned%20Aerial%20Vehicle%20%28UAV%29%20for%20its%20conversion%20into%20an%20operational%20laboratory%20platform%20%28INTERNATIONAL%20JOURNAL%20OF%20APPLIED%20ENGINEERING%20RESEARCH%29.pdf
Vancouver
White P, Vaca J, Villalba J, Martinez D, Pardo G, Cerón Muñoz HD. Redesign of an experimental Unmanned Aerial Vehicle (UAV) for its conversion into an operational laboratory platform [Internet]. International Journal of Applied Enginering Research. 2018 ; 13( 23): 16438-16446.[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/b4c197e2-f162-4d99-a5bc-8ea9e8b28e47/artigo%2003%20-%20Redesign%20of%20an%20experimental%20Unmanned%20Aerial%20Vehicle%20%28UAV%29%20for%20its%20conversion%20into%20an%20operational%20laboratory%20platform%20%28INTERNATIONAL%20JOURNAL%20OF%20APPLIED%20ENGINEERING%20RESEARCH%29.pdf
Trabalho de evento
Design and performance assessment of an inverted rectangular dorsal intake for military aviation (2018)
Bravo Mosquera, Pedro David; Abdalla, Alvaro Martins ; Cerón Muñoz, Hernán Darío ; Catalano, Fernando Martini
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AERONAVES MILITARES, FUSELAGEM 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. Design and performance assessment of an inverted rectangular dorsal intake for military aviation. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/f61f0f51-4199-4f6a-af2a-132b70c86bd1/trabalho%2003%20-%20DESIGN%20AND%20PERFORMANCE%20ASSESSMENT%20OF%20AN%20INVERTED%20RECTANGULAR%20DORSAL%20INTAKE%20FOR%20MILITARY%20AVIATION%20%28ICAS%202018%29.pdf. Acesso em: 30 set. 2024.
APA
Bravo Mosquera, P. D., Abdalla, A. M., Cerón Muñoz, H. D., & Catalano, F. M. (2018). Design and performance assessment of an inverted rectangular dorsal intake for military aviation. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/f61f0f51-4199-4f6a-af2a-132b70c86bd1/trabalho%2003%20-%20DESIGN%20AND%20PERFORMANCE%20ASSESSMENT%20OF%20AN%20INVERTED%20RECTANGULAR%20DORSAL%20INTAKE%20FOR%20MILITARY%20AVIATION%20%28ICAS%202018%29.pdf
NLM
Bravo Mosquera PD, Abdalla AM, Cerón Muñoz HD, Catalano FM. Design and performance assessment of an inverted rectangular dorsal intake for military aviation [Internet]. Proceedings. 2018 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/f61f0f51-4199-4f6a-af2a-132b70c86bd1/trabalho%2003%20-%20DESIGN%20AND%20PERFORMANCE%20ASSESSMENT%20OF%20AN%20INVERTED%20RECTANGULAR%20DORSAL%20INTAKE%20FOR%20MILITARY%20AVIATION%20%28ICAS%202018%29.pdf
Vancouver
Bravo Mosquera PD, Abdalla AM, Cerón Muñoz HD, Catalano FM. Design and performance assessment of an inverted rectangular dorsal intake for military aviation [Internet]. Proceedings. 2018 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/f61f0f51-4199-4f6a-af2a-132b70c86bd1/trabalho%2003%20-%20DESIGN%20AND%20PERFORMANCE%20ASSESSMENT%20OF%20AN%20INVERTED%20RECTANGULAR%20DORSAL%20INTAKE%20FOR%20MILITARY%20AVIATION%20%28ICAS%202018%29.pdf
Trabalho de evento
Experimental and computational analysis of a UAV for superficial volcano surveillance (2018)
Bravo Mosquera, Pedro David; Botero Bolívar, Laura; Acevedo Giraldo, Daniel; Cerón Muñoz, Hernán Darío ; Catalano, Fernando Martini
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AERONAVES NÃO TRIPULADAS, 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. Experimental and computational analysis of a UAV for superficial volcano surveillance. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/84ca0c03-3933-4ac3-acb9-e79514b8bd96/trabalho%2015%20-%20EXPERIMENTAL%20AND%20COMPUTATIONAL%20ANALYSIS%20OF%20A%20UAV%20FOR%20SUPERFICIAL%20VOLCANO%20SURVEILLANCE%20%28ICAS%202018%29.pdf. Acesso em: 30 set. 2024.
APA
Bravo Mosquera, P. D., Botero Bolívar, L., Acevedo Giraldo, D., Cerón Muñoz, H. D., & Catalano, F. M. (2018). Experimental and computational analysis of a UAV for superficial volcano surveillance. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/84ca0c03-3933-4ac3-acb9-e79514b8bd96/trabalho%2015%20-%20EXPERIMENTAL%20AND%20COMPUTATIONAL%20ANALYSIS%20OF%20A%20UAV%20FOR%20SUPERFICIAL%20VOLCANO%20SURVEILLANCE%20%28ICAS%202018%29.pdf
NLM
Bravo Mosquera PD, Botero Bolívar L, Acevedo Giraldo D, Cerón Muñoz HD, Catalano FM. Experimental and computational analysis of a UAV for superficial volcano surveillance [Internet]. Proceedings. 2018 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/84ca0c03-3933-4ac3-acb9-e79514b8bd96/trabalho%2015%20-%20EXPERIMENTAL%20AND%20COMPUTATIONAL%20ANALYSIS%20OF%20A%20UAV%20FOR%20SUPERFICIAL%20VOLCANO%20SURVEILLANCE%20%28ICAS%202018%29.pdf
Vancouver
Bravo Mosquera PD, Botero Bolívar L, Acevedo Giraldo D, Cerón Muñoz HD, Catalano FM. Experimental and computational analysis of a UAV for superficial volcano surveillance [Internet]. Proceedings. 2018 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/84ca0c03-3933-4ac3-acb9-e79514b8bd96/trabalho%2015%20-%20EXPERIMENTAL%20AND%20COMPUTATIONAL%20ANALYSIS%20OF%20A%20UAV%20FOR%20SUPERFICIAL%20VOLCANO%20SURVEILLANCE%20%28ICAS%202018%29.pdf
Trabalho de evento
Caracterização de sensores digitais de pressão diferencial de baixo custo e sua implementação conceitual em um sistema de aquisição de dados manométricos (2018)
Lanaro, Lucca Real Bispo; Cerón Muñoz, Hernán Darío
Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC
Subjects: INTERNET DAS COISAS, TELEMETRIA, MICROELETRÔNICA, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
LANARO, Lucca Real Bispo e CERÓN MUÑOZ, Hernán Darío. Caracterização de sensores digitais de pressão diferencial de baixo custo e sua implementação conceitual em um sistema de aquisição de dados manométricos. 2018, Anais.. São Carlos, SP: EESC-USP, 2018. Disponível em: http://soac.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1370/829. Acesso em: 30 set. 2024.
APA
Lanaro, L. R. B., & Cerón Muñoz, H. D. (2018). Caracterização de sensores digitais de pressão diferencial de baixo custo e sua implementação conceitual em um sistema de aquisição de dados manométricos. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1370/829
NLM
Lanaro LRB, Cerón Muñoz HD. Caracterização de sensores digitais de pressão diferencial de baixo custo e sua implementação conceitual em um sistema de aquisição de dados manométricos [Internet]. Anais. 2018 ;[citado 2024 set. 30 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1370/829
Vancouver
Lanaro LRB, Cerón Muñoz HD. Caracterização de sensores digitais de pressão diferencial de baixo custo e sua implementação conceitual em um sistema de aquisição de dados manométricos [Internet]. Anais. 2018 ;[citado 2024 set. 30 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1370/829
Trabalho de evento
Damage classification based on machine learning applications for an unmanned aerial vehicle (2017)
Anaya, Maribel; Cerón Muñoz, Hernán Darío ; Vitola, Jaime; Tibaduiza, D. A.; Pozo, F.
Source: Proceedings. Conference titles: International Workshop on Structural Health Monitoring. Unidade: EESC
Subjects: AERONAVES NÃO TRIPULADAS, ROBÓTICA, ASAS DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
ANAYA, Maribel et al. Damage classification based on machine learning applications for an unmanned aerial vehicle. 2017, Anais.. Stanford, CA, USA: Stanford University, 2017. Disponível em: https://repositorio.usp.br/directbitstream/8def7de2-b4c3-4430-81be-eeb78bd1b7ce/trabalho%2012%20-%20Damage%20classification%20based%20on%20machine%20learning%20applications%20for%20an%20unmanned%20aerial%20vehicle%20%28The%2011th%20International%20Workshop%20on%20Structural%20Health%20Monitoring%202017%29.pdf. Acesso em: 30 set. 2024.
APA
Anaya, M., Cerón Muñoz, H. D., Vitola, J., Tibaduiza, D. A., & Pozo, F. (2017). Damage classification based on machine learning applications for an unmanned aerial vehicle. In Proceedings. Stanford, CA, USA: Stanford University. Recuperado de https://repositorio.usp.br/directbitstream/8def7de2-b4c3-4430-81be-eeb78bd1b7ce/trabalho%2012%20-%20Damage%20classification%20based%20on%20machine%20learning%20applications%20for%20an%20unmanned%20aerial%20vehicle%20%28The%2011th%20International%20Workshop%20on%20Structural%20Health%20Monitoring%202017%29.pdf
NLM
Anaya M, Cerón Muñoz HD, Vitola J, Tibaduiza DA, Pozo F. Damage classification based on machine learning applications for an unmanned aerial vehicle [Internet]. Proceedings. 2017 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/8def7de2-b4c3-4430-81be-eeb78bd1b7ce/trabalho%2012%20-%20Damage%20classification%20based%20on%20machine%20learning%20applications%20for%20an%20unmanned%20aerial%20vehicle%20%28The%2011th%20International%20Workshop%20on%20Structural%20Health%20Monitoring%202017%29.pdf
Vancouver
Anaya M, Cerón Muñoz HD, Vitola J, Tibaduiza DA, Pozo F. Damage classification based on machine learning applications for an unmanned aerial vehicle [Internet]. Proceedings. 2017 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/8def7de2-b4c3-4430-81be-eeb78bd1b7ce/trabalho%2012%20-%20Damage%20classification%20based%20on%20machine%20learning%20applications%20for%20an%20unmanned%20aerial%20vehicle%20%28The%2011th%20International%20Workshop%20on%20Structural%20Health%20Monitoring%202017%29.pdf

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