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Artigo de periodico
Predicting airfoil dynamic stall loads using neural networks (2025)
Camacho, Emanuel A. R. ; Silva, Andre R. R. ; Marques, Flavio Donizeti
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: INTELIGÊNCIA ARTIFICIAL, AEROFÓLIOS, AERODINÂMICA DE AERONAVES, ENGENHARIA MECÂNICA
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ABNT
CAMACHO, Emanuel A. R. e SILVA, Andre R. R. e MARQUES, Flavio Donizeti. Predicting airfoil dynamic stall loads using neural networks. Aerospace Science and Technology, v. 165, p. 1-10, 2025Tradução . . Disponível em: http://dx.doi.org/10.1016/j.ast.2025.110466. Acesso em: 25 jan. 2026.
APA
Camacho, E. A. R., Silva, A. R. R., & Marques, F. D. (2025). Predicting airfoil dynamic stall loads using neural networks. Aerospace Science and Technology, 165, 1-10. doi:10.1016/j.ast.2025.110466
NLM
Camacho EAR, Silva ARR, Marques FD. Predicting airfoil dynamic stall loads using neural networks [Internet]. Aerospace Science and Technology. 2025 ; 165 1-10.[citado 2026 jan. 25 ] Available from: http://dx.doi.org/10.1016/j.ast.2025.110466
Vancouver
Camacho EAR, Silva ARR, Marques FD. Predicting airfoil dynamic stall loads using neural networks [Internet]. Aerospace Science and Technology. 2025 ; 165 1-10.[citado 2026 jan. 25 ] Available from: http://dx.doi.org/10.1016/j.ast.2025.110466
Artigo de periodico
A proposed methodology for diverterless supersonic inlet aerodynamic integration with a generic forebody (2025)
Vaca Rios, John Jairo ; Cerón Muñoz, Hernán Darío
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, PROPULSÃO DE AERONAVES, DINÂMICA DOS FLUÍDOS COMPUTACIONAL, ENGENHARIA AERONÁUTICA
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ABNT
VACA RIOS, John Jairo e CERÓN MUÑOZ, Hernán Darío. A proposed methodology for diverterless supersonic inlet aerodynamic integration with a generic forebody. Aerospace Science and Technology, v. 161, p. 1-14, 2025Tradução . . Disponível em: http://dx.doi.org/10.1016/j.ast.2025.110135. Acesso em: 25 jan. 2026.
APA
Vaca Rios, J. J., & Cerón Muñoz, H. D. (2025). A proposed methodology for diverterless supersonic inlet aerodynamic integration with a generic forebody. Aerospace Science and Technology, 161, 1-14. doi:10.1016/j.ast.2025.110135
NLM
Vaca Rios JJ, Cerón Muñoz HD. A proposed methodology for diverterless supersonic inlet aerodynamic integration with a generic forebody [Internet]. Aerospace Science and Technology. 2025 ; 161 1-14.[citado 2026 jan. 25 ] Available from: http://dx.doi.org/10.1016/j.ast.2025.110135
Vancouver
Vaca Rios JJ, Cerón Muñoz HD. A proposed methodology for diverterless supersonic inlet aerodynamic integration with a generic forebody [Internet]. Aerospace Science and Technology. 2025 ; 161 1-14.[citado 2026 jan. 25 ] Available from: http://dx.doi.org/10.1016/j.ast.2025.110135
Artigo de periodico
Aeroelastic effects in PIO occurrences: A dual approach on flight simulator tests (2024)
Paladini, Andre Luis Aguiar; Drewiacki, Daniel; Bidinotto, Jorge Henrique
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, SIMULADORES DE VOO, ALGORITMOS, ENGENHARIA AERONÁUTICA
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PALADINI, Andre Luis Aguiar e DREWIACKI, Daniel e BIDINOTTO, Jorge Henrique. Aeroelastic effects in PIO occurrences: A dual approach on flight simulator tests. Aerospace Science and Technology, v. 151, p. 1-12, 2024Tradução . . Disponível em: http://dx.doi.org/10.1016/j.ast.2024.109337. Acesso em: 25 jan. 2026.
APA
Paladini, A. L. A., Drewiacki, D., & Bidinotto, J. H. (2024). Aeroelastic effects in PIO occurrences: A dual approach on flight simulator tests. Aerospace Science and Technology, 151, 1-12. doi:10.1016/j.ast.2024.109337
NLM
Paladini ALA, Drewiacki D, Bidinotto JH. Aeroelastic effects in PIO occurrences: A dual approach on flight simulator tests [Internet]. Aerospace Science and Technology. 2024 ; 151 1-12.[citado 2026 jan. 25 ] Available from: http://dx.doi.org/10.1016/j.ast.2024.109337
Vancouver
Paladini ALA, Drewiacki D, Bidinotto JH. Aeroelastic effects in PIO occurrences: A dual approach on flight simulator tests [Internet]. Aerospace Science and Technology. 2024 ; 151 1-12.[citado 2026 jan. 25 ] Available from: http://dx.doi.org/10.1016/j.ast.2024.109337
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
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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: 25 jan. 2026.
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 2026 jan. 25 ] 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 2026 jan. 25 ] Available from: https://doi.org/10.1016/j.ast.2019.105542
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: 25 jan. 2026.
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 2026 jan. 25 ] 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 2026 jan. 25 ] Available from: https://doi.org/10.1016/j.ast.2019.105642
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: 25 jan. 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 jan. 25 ] 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 jan. 25 ] Available from: https://doi.org/10.1016/j.ast.2019.01.059
Artigo de periodico
Aeroelastic tailoring of nonlinear typical section using the method of multiple scales to predict post-flutter stable LCOs (2019)
Sanches, Leonardo ; Guimarães, Thiago A. M; Marques, Flavio Donizeti
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA
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ABNT
SANCHES, Leonardo e GUIMARÃES, Thiago A. M e MARQUES, Flavio Donizeti. Aeroelastic tailoring of nonlinear typical section using the method of multiple scales to predict post-flutter stable LCOs. Aerospace Science and Technology, v. 90, p. 157-168, 2019Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2019.04.031. Acesso em: 25 jan. 2026.
APA
Sanches, L., Guimarães, T. A. M., & Marques, F. D. (2019). Aeroelastic tailoring of nonlinear typical section using the method of multiple scales to predict post-flutter stable LCOs. Aerospace Science and Technology, 90, 157-168. doi:10.1016/j.ast.2019.04.031
NLM
Sanches L, Guimarães TAM, Marques FD. Aeroelastic tailoring of nonlinear typical section using the method of multiple scales to predict post-flutter stable LCOs [Internet]. Aerospace Science and Technology. 2019 ; 90 157-168.[citado 2026 jan. 25 ] Available from: https://doi.org/10.1016/j.ast.2019.04.031
Vancouver
Sanches L, Guimarães TAM, Marques FD. Aeroelastic tailoring of nonlinear typical section using the method of multiple scales to predict post-flutter stable LCOs [Internet]. Aerospace Science and Technology. 2019 ; 90 157-168.[citado 2026 jan. 25 ] Available from: https://doi.org/10.1016/j.ast.2019.04.031
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: 25 jan. 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 jan. 25 ] 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 jan. 25 ] 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
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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: 25 jan. 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 jan. 25 ] 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 jan. 25 ] Available from: https://doi.org/10.1016/j.ast.2017.09.005
Artigo de periodico
Effects of combined hardening and free-play nonlinearities on the response of a typical aeroelastic section (2016)
Pereira, Daniel de Almeida; Vasconcellos, Rui Marcos Grombone de; Hajj, Muhammad R.; Marques, Flavio Donizeti
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: VIBRAÇÕES DE AERONAVES, TEORIA DA BIFURCAÇÃO, AEROELASTICIDADE DE AERONAVES
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ABNT
PEREIRA, Daniel de Almeida et al. Effects of combined hardening and free-play nonlinearities on the response of a typical aeroelastic section. Aerospace Science and Technology, v. 50, p. 44-54, 2016Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2015.12.022. Acesso em: 25 jan. 2026.
APA
Pereira, D. de A., Vasconcellos, R. M. G. de, Hajj, M. R., & Marques, F. D. (2016). Effects of combined hardening and free-play nonlinearities on the response of a typical aeroelastic section. Aerospace Science and Technology, 50, 44-54. doi:10.1016/j.ast.2015.12.022
NLM
Pereira D de A, Vasconcellos RMG de, Hajj MR, Marques FD. Effects of combined hardening and free-play nonlinearities on the response of a typical aeroelastic section [Internet]. Aerospace Science and Technology. 2016 ; 50 44-54.[citado 2026 jan. 25 ] Available from: https://doi.org/10.1016/j.ast.2015.12.022
Vancouver
Pereira D de A, Vasconcellos RMG de, Hajj MR, Marques FD. Effects of combined hardening and free-play nonlinearities on the response of a typical aeroelastic section [Internet]. Aerospace Science and Technology. 2016 ; 50 44-54.[citado 2026 jan. 25 ] Available from: https://doi.org/10.1016/j.ast.2015.12.022
Artigo de periodico
Virtual boundary method for inviscid transonic flow over supercritical airfoils (2016)
Solarte Pineda, Jhonathan; Greco Júnior, Paulo Celso
Source: Aerospace Science and Technology. Unidade: EESC
Assunto: AERODINÂMICA DE AERONAVES
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ABNT
SOLARTE PINEDA, Jhonathan e GRECO JÚNIOR, Paulo Celso. Virtual boundary method for inviscid transonic flow over supercritical airfoils. Aerospace Science and Technology, v. No 2016, p. 380-388, 2016Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2016.08.024. Acesso em: 25 jan. 2026.
APA
Solarte Pineda, J., & Greco Júnior, P. C. (2016). Virtual boundary method for inviscid transonic flow over supercritical airfoils. Aerospace Science and Technology, No 2016, 380-388. doi:10.1016/j.ast.2016.08.024
NLM
Solarte Pineda J, Greco Júnior PC. Virtual boundary method for inviscid transonic flow over supercritical airfoils [Internet]. Aerospace Science and Technology. 2016 ; No 2016 380-388.[citado 2026 jan. 25 ] Available from: https://doi.org/10.1016/j.ast.2016.08.024
Vancouver
Solarte Pineda J, Greco Júnior PC. Virtual boundary method for inviscid transonic flow over supercritical airfoils [Internet]. Aerospace Science and Technology. 2016 ; No 2016 380-388.[citado 2026 jan. 25 ] Available from: https://doi.org/10.1016/j.ast.2016.08.024
Artigo de periodico
Effect of an excrescence in the slat cove: flow-field, acoustic radiation and coherent structures (2015)
Souza, Daniel Sampaio; Rodríguez Álvarez, Daniel; Simões, Leandro Guilherme Crenite; Medeiros, Marcello Augusto Faraco de
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: ATERRISSAGEM, ACÚSTICA, AERONAVES
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ABNT
SOUZA, Daniel Sampaio et al. Effect of an excrescence in the slat cove: flow-field, acoustic radiation and coherent structures. Aerospace Science and Technology, v. 44, p. 108-115, 2015Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2015.01.016. Acesso em: 25 jan. 2026.
APA
Souza, D. S., Rodríguez Álvarez, D., Simões, L. G. C., & Medeiros, M. A. F. de. (2015). Effect of an excrescence in the slat cove: flow-field, acoustic radiation and coherent structures. Aerospace Science and Technology, 44, 108-115. doi:10.1016/j.ast.2015.01.016
NLM
Souza DS, Rodríguez Álvarez D, Simões LGC, Medeiros MAF de. Effect of an excrescence in the slat cove: flow-field, acoustic radiation and coherent structures [Internet]. Aerospace Science and Technology. 2015 ; 44 108-115.[citado 2026 jan. 25 ] Available from: https://doi.org/10.1016/j.ast.2015.01.016
Vancouver
Souza DS, Rodríguez Álvarez D, Simões LGC, Medeiros MAF de. Effect of an excrescence in the slat cove: flow-field, acoustic radiation and coherent structures [Internet]. Aerospace Science and Technology. 2015 ; 44 108-115.[citado 2026 jan. 25 ] Available from: https://doi.org/10.1016/j.ast.2015.01.016
Artigo de periodico
Compressible modes in a square lid-driven cavity (2015)
Bergamo, Leandro Fernandes; Gennaro, Elmer Mateus; Theofilis, Vassilis; Medeiros, Marcello Augusto Faraco de
Source: Aerospace Science and Technology. Unidade: EESC
Assunto: AERODINÂMICA DE AERONAVES
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ABNT
BERGAMO, Leandro Fernandes et al. Compressible modes in a square lid-driven cavity. Aerospace Science and Technology, v. 44, p. 125-134, 2015Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2015.03.010. Acesso em: 25 jan. 2026.
APA
Bergamo, L. F., Gennaro, E. M., Theofilis, V., & Medeiros, M. A. F. de. (2015). Compressible modes in a square lid-driven cavity. Aerospace Science and Technology, 44, 125-134. doi:10.1016/j.ast.2015.03.010
NLM
Bergamo LF, Gennaro EM, Theofilis V, Medeiros MAF de. Compressible modes in a square lid-driven cavity [Internet]. Aerospace Science and Technology. 2015 ; 44 125-134.[citado 2026 jan. 25 ] Available from: https://doi.org/10.1016/j.ast.2015.03.010
Vancouver
Bergamo LF, Gennaro EM, Theofilis V, Medeiros MAF de. Compressible modes in a square lid-driven cavity [Internet]. Aerospace Science and Technology. 2015 ; 44 125-134.[citado 2026 jan. 25 ] Available from: https://doi.org/10.1016/j.ast.2015.03.010
Artigo de periodico
On the controversy regarding the effect of flow shear on the Strouhal number of cylinder vortex shedding (2013)
Gennaro, Elmer Mateus; Colaciti, Alysson Kennerly; Medeiros, Marcello Augusto Faraco de
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: HIDRODINÂMICA, EQUAÇÕES
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ABNT
GENNARO, Elmer Mateus e COLACITI, Alysson Kennerly e MEDEIROS, Marcello Augusto Faraco de. On the controversy regarding the effect of flow shear on the Strouhal number of cylinder vortex shedding. Aerospace Science and Technology, v. 29, n. 1, p. 313-320, 2013Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2013.04.002. Acesso em: 25 jan. 2026.
APA
Gennaro, E. M., Colaciti, A. K., & Medeiros, M. A. F. de. (2013). On the controversy regarding the effect of flow shear on the Strouhal number of cylinder vortex shedding. Aerospace Science and Technology, 29( 1), 313-320. doi:10.1016/j.ast.2013.04.002
NLM
Gennaro EM, Colaciti AK, Medeiros MAF de. On the controversy regarding the effect of flow shear on the Strouhal number of cylinder vortex shedding [Internet]. Aerospace Science and Technology. 2013 ; 29( 1): 313-320.[citado 2026 jan. 25 ] Available from: https://doi.org/10.1016/j.ast.2013.04.002
Vancouver
Gennaro EM, Colaciti AK, Medeiros MAF de. On the controversy regarding the effect of flow shear on the Strouhal number of cylinder vortex shedding [Internet]. Aerospace Science and Technology. 2013 ; 29( 1): 313-320.[citado 2026 jan. 25 ] Available from: https://doi.org/10.1016/j.ast.2013.04.002
Artigo de periodico
Hopf bifurcation analysis of typical sections with structural nonlinearities in transonic flow (2013)
Camilo, Elizangela; Marques, Flavio Donizeti ; Azevedo, João Luiz Filgueiras de
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: SISTEMAS NÃO LINEARES, AERODINÂMICA DE AERONAVES
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ABNT
CAMILO, Elizangela e MARQUES, Flavio Donizeti e AZEVEDO, João Luiz Filgueiras de. Hopf bifurcation analysis of typical sections with structural nonlinearities in transonic flow. Aerospace Science and Technology, v. 30, n. 1, p. 163-174, 2013Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2013.07.013. Acesso em: 25 jan. 2026.
APA
Camilo, E., Marques, F. D., & Azevedo, J. L. F. de. (2013). Hopf bifurcation analysis of typical sections with structural nonlinearities in transonic flow. Aerospace Science and Technology, 30( 1), 163-174. doi:10.1016/j.ast.2013.07.013
NLM
Camilo E, Marques FD, Azevedo JLF de. Hopf bifurcation analysis of typical sections with structural nonlinearities in transonic flow [Internet]. Aerospace Science and Technology. 2013 ; 30( 1): 163-174.[citado 2026 jan. 25 ] Available from: https://doi.org/10.1016/j.ast.2013.07.013
Vancouver
Camilo E, Marques FD, Azevedo JLF de. Hopf bifurcation analysis of typical sections with structural nonlinearities in transonic flow [Internet]. Aerospace Science and Technology. 2013 ; 30( 1): 163-174.[citado 2026 jan. 25 ] Available from: https://doi.org/10.1016/j.ast.2013.07.013

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