A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
GONZALEZ-DEGREIFF, Pablo et al. Numerical and experimental analysis of the effect of wavy leading edge on stabilizer. Physics of fluids, v. 37, p. 1-22, 2025Tradução . . Disponível em: https://dx.doi.org/10.1063/5.0267295. Acesso em: 27 abr. 2026.
APA
Gonzalez-DeGreiff, P., Gomez Rivera, W., Bravo Mosquera, P. D., & Cerón Muñoz, H. D. (2025). Numerical and experimental analysis of the effect of wavy leading edge on stabilizer. Physics of fluids, 37, 1-22. doi:10.1063/5.0267295
NLM
Gonzalez-DeGreiff P, Gomez Rivera W, Bravo Mosquera PD, Cerón Muñoz HD. Numerical and experimental analysis of the effect of wavy leading edge on stabilizer [Internet]. Physics of fluids. 2025 ; 37 1-22.[citado 2026 abr. 27 ] Available from: https://dx.doi.org/10.1063/5.0267295
Vancouver
Gonzalez-DeGreiff P, Gomez Rivera W, Bravo Mosquera PD, Cerón Muñoz HD. Numerical and experimental analysis of the effect of wavy leading edge on stabilizer [Internet]. Physics of fluids. 2025 ; 37 1-22.[citado 2026 abr. 27 ] Available from: https://dx.doi.org/10.1063/5.0267295
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: 27 abr. 2026.
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 2026 abr. 27 ] 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 2026 abr. 27 ] Available from: https://doi.org/10.3390/aerospace10070651
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://teses.usp.br/teses/disponiveis/18/18148/tde-19122022-155409/. Acesso em: 27 abr. 2026.
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://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 2026 abr. 27 ] Available from: https://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 2026 abr. 27 ] Available from: https://teses.usp.br/teses/disponiveis/18/18148/tde-19122022-155409/
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BRAVO MOSQUERA, Pedro David e CATALANO, Fernando Martini e ZINGG, David W. Unconventional aircraft for civil aviation. Progress in Aerospace Sciences, v. 131, p. 1-29, 2022Tradução . . Disponível em: https://doi.org/10.1016/j.paerosci.2022.100813. Acesso em: 27 abr. 2026.
APA
Bravo Mosquera, P. D., Catalano, F. M., & Zingg, D. W. (2022). Unconventional aircraft for civil aviation. Progress in Aerospace Sciences, 131, 1-29. doi:10.1016/j.paerosci.2022.100813
NLM
Bravo Mosquera PD, Catalano FM, Zingg DW. Unconventional aircraft for civil aviation [Internet]. Progress in Aerospace Sciences. 2022 ; 131 1-29.[citado 2026 abr. 27 ] Available from: https://doi.org/10.1016/j.paerosci.2022.100813
Vancouver
Bravo Mosquera PD, Catalano FM, Zingg DW. Unconventional aircraft for civil aviation [Internet]. Progress in Aerospace Sciences. 2022 ; 131 1-29.[citado 2026 abr. 27 ] Available from: https://doi.org/10.1016/j.paerosci.2022.100813
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. 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: 27 abr. 2026.
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 2026 abr. 27 ] 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 2026 abr. 27 ] Available from: https://doi.org/10.1007/s40430-022-03924-x
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 27 abr. 2026.
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 2026 abr. 27 ] 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 2026 abr. 27 ] 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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BOCCATO, Bruno Ribeiro e BRAVO MOSQUERA, Pedro David e CATALANO, Fernando Martini. Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-4200. Acesso em: 27 abr. 2026.
APA
Boccato, B. R., Bravo Mosquera, P. D., & Catalano, F. M. (2019). Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-4200
NLM
Boccato BR, Bravo Mosquera PD, Catalano FM. Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake [Internet]. Proceedings. 2019 ;[citado 2026 abr. 27 ] Available from: https://doi.org/10.2514/6.2019-4200
Vancouver
Boccato BR, Bravo Mosquera PD, Catalano FM. Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake [Internet]. Proceedings. 2019 ;[citado 2026 abr. 27 ] Available from: https://doi.org/10.2514/6.2019-4200
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. 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: 27 abr. 2026.
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 2026 abr. 27 ] 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 2026 abr. 27 ] Available from: https://doi.org/10.2514/6.2019-3850
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: 27 abr. 2026.
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 2026 abr. 27 ] 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 2026 abr. 27 ] Available from: https://doi.org/10.1016/j.ast.2019.01.059
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 27 abr. 2026.
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 2026 abr. 27 ] 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 2026 abr. 27 ] 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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BRAVO MOSQUERA, Pedro David e ABDALLA, Alvaro Martins e CATALANO, Fernando Martini. Evaluation of delta wing effects on the stealth-aerodynamic features for non-conventional fighter aircraft. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/d5e79d68-cf3c-49f9-acbe-477649c98a5f/trabalho%2013%20-%20EVALUATION%20OF%20DELTA%20WING%20EFFECTS%20ON%20THE%20STEALTH-AERODYNAMIC%20FEATURES%20FOR%20NON-CONVENTIONAL%20FIGHTER%20AIRCRAFT%20%28ICAS%202018%29.pdf. Acesso em: 27 abr. 2026.
APA
Bravo Mosquera, P. D., Abdalla, A. M., & Catalano, F. M. (2018). Evaluation of delta wing effects on the stealth-aerodynamic features for non-conventional fighter aircraft. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/d5e79d68-cf3c-49f9-acbe-477649c98a5f/trabalho%2013%20-%20EVALUATION%20OF%20DELTA%20WING%20EFFECTS%20ON%20THE%20STEALTH-AERODYNAMIC%20FEATURES%20FOR%20NON-CONVENTIONAL%20FIGHTER%20AIRCRAFT%20%28ICAS%202018%29.pdf
NLM
Bravo Mosquera PD, Abdalla AM, Catalano FM. Evaluation of delta wing effects on the stealth-aerodynamic features for non-conventional fighter aircraft [Internet]. Proceedings. 2018 ;[citado 2026 abr. 27 ] Available from: https://repositorio.usp.br/directbitstream/d5e79d68-cf3c-49f9-acbe-477649c98a5f/trabalho%2013%20-%20EVALUATION%20OF%20DELTA%20WING%20EFFECTS%20ON%20THE%20STEALTH-AERODYNAMIC%20FEATURES%20FOR%20NON-CONVENTIONAL%20FIGHTER%20AIRCRAFT%20%28ICAS%202018%29.pdf
Vancouver
Bravo Mosquera PD, Abdalla AM, Catalano FM. Evaluation of delta wing effects on the stealth-aerodynamic features for non-conventional fighter aircraft [Internet]. Proceedings. 2018 ;[citado 2026 abr. 27 ] Available from: https://repositorio.usp.br/directbitstream/d5e79d68-cf3c-49f9-acbe-477649c98a5f/trabalho%2013%20-%20EVALUATION%20OF%20DELTA%20WING%20EFFECTS%20ON%20THE%20STEALTH-AERODYNAMIC%20FEATURES%20FOR%20NON-CONVENTIONAL%20FIGHTER%20AIRCRAFT%20%28ICAS%202018%29.pdf
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: 27 abr. 2026.
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 2026 abr. 27 ] 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 2026 abr. 27 ] 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
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: 27 abr. 2026.
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 2026 abr. 27 ] 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 2026 abr. 27 ] Available from: https://doi.org/10.1016/j.ast.2018.07.014
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: 27 abr. 2026.
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 2026 abr. 27 ] 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 2026 abr. 27 ] 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
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: 27 abr. 2026.
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 2026 abr. 27 ] 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 2026 abr. 27 ] 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
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: 27 abr. 2026.
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 2026 abr. 27 ] 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 2026 abr. 27 ] Available from: https://doi.org/10.1016/j.ast.2017.09.005
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
PEDRAZA BETANCOURTH, Nelson Javier et al. Design and manufacture of a solar-powered unmanned aerial vehicle for civilian surveillance missions. Journal of Aerospace Technology and Management, v. 8, n. 4, p. 385-396, 2016Tradução . . Disponível em: https://doi.org/10.5028/jatm.v8i4.678. Acesso em: 27 abr. 2026.
APA
Pedraza Betancourth, N. J., Parra Villamarin, J. E., Vaca Rios, J. J., Bravo Mosquera, P. D., & Cerón Muñoz, H. D. (2016). Design and manufacture of a solar-powered unmanned aerial vehicle for civilian surveillance missions. Journal of Aerospace Technology and Management, 8( 4), 385-396. doi:10.5028/jatm.v8i4.678
NLM
Pedraza Betancourth NJ, Parra Villamarin JE, Vaca Rios JJ, Bravo Mosquera PD, Cerón Muñoz HD. Design and manufacture of a solar-powered unmanned aerial vehicle for civilian surveillance missions [Internet]. Journal of Aerospace Technology and Management. 2016 ; 8( 4): 385-396.[citado 2026 abr. 27 ] Available from: https://doi.org/10.5028/jatm.v8i4.678
Vancouver
Pedraza Betancourth NJ, Parra Villamarin JE, Vaca Rios JJ, Bravo Mosquera PD, Cerón Muñoz HD. Design and manufacture of a solar-powered unmanned aerial vehicle for civilian surveillance missions [Internet]. Journal of Aerospace Technology and Management. 2016 ; 8( 4): 385-396.[citado 2026 abr. 27 ] Available from: https://doi.org/10.5028/jatm.v8i4.678
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BRAVO MOSQUERA, Pedro David et al. Conceptual and aerodynamic design of a UAV for superficial volcano monitoring. 2016, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2016. . Acesso em: 27 abr. 2026.
APA
Bravo Mosquera, P. D., Abdalla, A. M., Cerón Muñoz, H. D., & Catalano, F. M. (2016). Conceptual and aerodynamic design of a UAV for superficial volcano monitoring. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Bravo Mosquera PD, Abdalla AM, Cerón Muñoz HD, Catalano FM. Conceptual and aerodynamic design of a UAV for superficial volcano monitoring. Proceedings. 2016 ;[citado 2026 abr. 27 ]
Vancouver
Bravo Mosquera PD, Abdalla AM, Cerón Muñoz HD, Catalano FM. Conceptual and aerodynamic design of a UAV for superficial volcano monitoring. Proceedings. 2016 ;[citado 2026 abr. 27 ]
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CERÓN MUÑOZ, Hernán Darío et al. Experimental analyses of droop, wingtips and fences on a BWB model. 2016, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2016. . Acesso em: 27 abr. 2026.
APA
Cerón Muñoz, H. D., Diaz Izquierdo, D. O., Bravo Mosquera, P. D., & Catalano, F. M. (2016). Experimental analyses of droop, wingtips and fences on a BWB model. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Cerón Muñoz HD, Diaz Izquierdo DO, Bravo Mosquera PD, Catalano FM. Experimental analyses of droop, wingtips and fences on a BWB model. Proceedings. 2016 ;[citado 2026 abr. 27 ]
Vancouver
Cerón Muñoz HD, Diaz Izquierdo DO, Bravo Mosquera PD, Catalano FM. Experimental analyses of droop, wingtips and fences on a BWB model. Proceedings. 2016 ;[citado 2026 abr. 27 ]
; Gomez Rivera, William 
