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Trabalho de evento
Accurate CFD measurements of vortex generators effects on a wing subject to shock-induced separation (2021)
Ferrari, Marcello; Morais, Kelvin C; Ferrari, Denise; Resende, Otto C. de; Santos, Luis Carlos de Castro
Source: Proceedings. Conference titles: AIAA Scitech Forum. Unidade: IME
Subjects: DINÂMICA DOS FLUÍDOS, MODELOS MATEMÁTICOS
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ABNT
FERRARI, Marcello et al. Accurate CFD measurements of vortex generators effects on a wing subject to shock-induced separation. 2021, Anais.. Reston, VA, USA: AIAA, 2021. Disponível em: https://doi.org/10.2514/6.2021-1839. Acesso em: 29 nov. 2025.
APA
Ferrari, M., Morais, K. C., Ferrari, D., Resende, O. C. de, & Santos, L. C. de C. (2021). Accurate CFD measurements of vortex generators effects on a wing subject to shock-induced separation. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2021-1839
NLM
Ferrari M, Morais KC, Ferrari D, Resende OC de, Santos LC de C. Accurate CFD measurements of vortex generators effects on a wing subject to shock-induced separation [Internet]. Proceedings. 2021 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2021-1839
Vancouver
Ferrari M, Morais KC, Ferrari D, Resende OC de, Santos LC de C. Accurate CFD measurements of vortex generators effects on a wing subject to shock-induced separation [Internet]. Proceedings. 2021 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2021-1839
Trabalho de evento
Loss of control in flight: comparing qualitative pilot opinion with quantitative flight data (2020)
Macedo, João Paulo Costa Antunes de; Bidinotto, Jorge Henrique ; Bromfield, Michael A.
Source: Proceedings. Conference titles: AIAA Aviation Forum. Unidade: EESC
Subjects: VOO (ENGENHARIA AERONÁUTICA), ACIDENTES, SIMULADORES DE VOO, ENGENHARIA AERONÁUTICA
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MACEDO, João Paulo Costa Antunes de e BIDINOTTO, Jorge Henrique e BROMFIELD, Michael A. Loss of control in flight: comparing qualitative pilot opinion with quantitative flight data. 2020, Anais.. Reston, VA, USA: AIAA, 2020. Disponível em: https://doi.org/10.2514/6.2020-2911. Acesso em: 29 nov. 2025.
APA
Macedo, J. P. C. A. de, Bidinotto, J. H., & Bromfield, M. A. (2020). Loss of control in flight: comparing qualitative pilot opinion with quantitative flight data. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2020-2911
NLM
Macedo JPCA de, Bidinotto JH, Bromfield MA. Loss of control in flight: comparing qualitative pilot opinion with quantitative flight data [Internet]. Proceedings. 2020 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2020-2911
Vancouver
Macedo JPCA de, Bidinotto JH, Bromfield MA. Loss of control in flight: comparing qualitative pilot opinion with quantitative flight data [Internet]. Proceedings. 2020 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2020-2911
Trabalho de evento
Aeroelastic analysis and characterization of three-degree-of-freedom systems with discontinuous nonlinearity (2020)
Vasconcellos, Rui Marcos Grombone de; Bouma, A.; Marques, Flavio Donizeti ; Abdelkefi, A.; Hajj, M. R.
Source: Proceedings. Conference titles: AIAA Aviation Forum. Unidade: EESC
Assunto: AEROELASTICIDADE DE AERONAVES
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VASCONCELLOS, Rui Marcos Grombone de et al. Aeroelastic analysis and characterization of three-degree-of-freedom systems with discontinuous nonlinearity. 2020, Anais.. Reston, VA, USA: AIAA, 2020. Disponível em: https://doi.org/10.2514/6.2020-2665. Acesso em: 29 nov. 2025.
APA
Vasconcellos, R. M. G. de, Bouma, A., Marques, F. D., Abdelkefi, A., & Hajj, M. R. (2020). Aeroelastic analysis and characterization of three-degree-of-freedom systems with discontinuous nonlinearity. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2020-2665
NLM
Vasconcellos RMG de, Bouma A, Marques FD, Abdelkefi A, Hajj MR. Aeroelastic analysis and characterization of three-degree-of-freedom systems with discontinuous nonlinearity [Internet]. Proceedings. 2020 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2020-2665
Vancouver
Vasconcellos RMG de, Bouma A, Marques FD, Abdelkefi A, Hajj MR. Aeroelastic analysis and characterization of three-degree-of-freedom systems with discontinuous nonlinearity [Internet]. Proceedings. 2020 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2020-2665
Trabalho de evento
Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake (2019)
Boccato, Bruno Ribeiro; Bravo Mosquera, Pedro David; Catalano, Fernando Martini
Source: Proceedings. Conference titles: AIAA Propulsion and Energy Forum. Unidade: EESC
Subjects: ENGENHARIA AERONÁUTICA, AERODINÂMICA DE AERONAVES
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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: 29 nov. 2025.
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 2025 nov. 29 ] 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 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-4200
Trabalho de evento
A study on the 3D effects of slat cove fillers (2019)
Reis, Danillo Cafaldo dos; Coelho, Eduardo L. C.; Pereira, Lourenço Tércio Lima; Catalano, Fernando Martini ; Lima, Leandro S. de M.
Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC
Subjects: ENGENHARIA AERONÁUTICA, AEROACÚSTICA, TERCEIRA DIMENSÃO
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ABNT
REIS, Danillo Cafaldo dos et al. A study on the 3D effects of slat cove fillers. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-2406. Acesso em: 29 nov. 2025.
APA
Reis, D. C. dos, Coelho, E. L. C., Pereira, L. T. L., Catalano, F. M., & Lima, L. S. de M. (2019). A study on the 3D effects of slat cove fillers. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-2406
NLM
Reis DC dos, Coelho ELC, Pereira LTL, Catalano FM, Lima LS de M. A study on the 3D effects of slat cove fillers [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-2406
Vancouver
Reis DC dos, Coelho ELC, Pereira LTL, Catalano FM, Lima LS de M. A study on the 3D effects of slat cove fillers [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-2406
Trabalho de evento
An experimental and numeric investigation towards a reliable acoustic pressure level estimate using phased-array techniques (2019)
Pagani Júnior, Carlos do Carmo; Caldas, Luciano Coutinho; Medeiros, Marcello Augusto Faraco de
Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC
Subjects: ENGENHARIA AERONÁUTICA, AEROACÚSTICA
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ABNT
PAGANI JÚNIOR, Carlos do Carmo e CALDAS, Luciano Coutinho e MEDEIROS, Marcello Augusto Faraco de. An experimental and numeric investigation towards a reliable acoustic pressure level estimate using phased-array techniques. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-2700. Acesso em: 29 nov. 2025.
APA
Pagani Júnior, C. do C., Caldas, L. C., & Medeiros, M. A. F. de. (2019). An experimental and numeric investigation towards a reliable acoustic pressure level estimate using phased-array techniques. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-2700
NLM
Pagani Júnior C do C, Caldas LC, Medeiros MAF de. An experimental and numeric investigation towards a reliable acoustic pressure level estimate using phased-array techniques [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-2700
Vancouver
Pagani Júnior C do C, Caldas LC, Medeiros MAF de. An experimental and numeric investigation towards a reliable acoustic pressure level estimate using phased-array techniques [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-2700
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: 29 nov. 2025.
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 2025 nov. 29 ] 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 2025 nov. 29 ] 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: 29 nov. 2025.
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 2025 nov. 29 ] 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 2025 nov. 29 ] 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
Trabalho de evento
Inlet liner design for a fan noise test rig (2019)
Spillere, André M. N.; Braga, Danilo S; Seki, Leonardo A.; Bonomo, Lucas A.; Cordioli, Julio A.; Rocamora Junior, Bernardo Martínez; Greco Júnior, Paulo Celso ; Reis, Danillo Cafaldo dos; Coelho, Eduardo L. C
Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC
Subjects: AEROACÚSTICA, ENGENHARIA AERONÁUTICA
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ABNT
SPILLERE, André M. N. et al. Inlet liner design for a fan noise test rig. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-2724. Acesso em: 29 nov. 2025.
APA
Spillere, A. M. N., Braga, D. S., Seki, L. A., Bonomo, L. A., Cordioli, J. A., Rocamora Junior, B. M., et al. (2019). Inlet liner design for a fan noise test rig. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-2724
NLM
Spillere AMN, Braga DS, Seki LA, Bonomo LA, Cordioli JA, Rocamora Junior BM, Greco Júnior PC, Reis DC dos, Coelho ELC. Inlet liner design for a fan noise test rig [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-2724
Vancouver
Spillere AMN, Braga DS, Seki LA, Bonomo LA, Cordioli JA, Rocamora Junior BM, Greco Júnior PC, Reis DC dos, Coelho ELC. Inlet liner design for a fan noise test rig [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-2724
Trabalho de evento
Parametric analysis of the influence of slat geometry on acoustic noise (2018)
Botero Bolívar, Laura; Pereira, Lourenço Tércio Lima; Acevedo Giraldo, Daniel; Catalano, Fernando Martini ; Reis, Danillo Cafaldo dos; Coelho, Eduardo L. C
Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC
Subjects: AEROACÚSTICA, SLATS, ENGENHARIA AERONÁUTICA
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ABNT
BOTERO BOLÍVAR, Laura et al. Parametric analysis of the influence of slat geometry on acoustic noise. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3593. Acesso em: 29 nov. 2025.
APA
Botero Bolívar, L., Pereira, L. T. L., Acevedo Giraldo, D., Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2018). Parametric analysis of the influence of slat geometry on acoustic noise. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3593
NLM
Botero Bolívar L, Pereira LTL, Acevedo Giraldo D, Catalano FM, Reis DC dos, Coelho ELC. Parametric analysis of the influence of slat geometry on acoustic noise [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-3593
Vancouver
Botero Bolívar L, Pereira LTL, Acevedo Giraldo D, Catalano FM, Reis DC dos, Coelho ELC. Parametric analysis of the influence of slat geometry on acoustic noise [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-3593
Trabalho de evento
Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear (2018)
Rego, Leandro Falcão Loureiro; Pereira, Lourenço Tércio Lima; Catalano, Fernando Martini ; Speth, R.; Bent, P.; Fregnani, J. A.
Source: Proceedings. Conference titles: AAIA Aerospace Sciences Meeting. Unidade: EESC
Subjects: TRENS DE POUSO, ENGENHARIA AERONÁUTICA, AERODINÂMICA DE AERONAVES, AEROACÚSTICA
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ABNT
REGO, Leandro Falcão Loureiro et al. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-0759. Acesso em: 29 nov. 2025.
APA
Rego, L. F. L., Pereira, L. T. L., Catalano, F. M., Speth, R., Bent, P., & Fregnani, J. A. (2018). Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-0759
NLM
Rego LFL, Pereira LTL, Catalano FM, Speth R, Bent P, Fregnani JA. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-0759
Vancouver
Rego LFL, Pereira LTL, Catalano FM, Speth R, Bent P, Fregnani JA. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-0759
Trabalho de evento
Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model (2018)
Acevedo Giraldo, Daniel; Botero Bolívar, Laura; Pereira, Lourenço Tércio Lima; Catalano, Fernando Martini ; Reis, Danillo Cafaldo dos; Coelho, Eduardo L. C
Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC
Subjects: FLAPS, AEROACÚSTICA, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
ACEVEDO GIRALDO, Daniel et al. Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3799. Acesso em: 29 nov. 2025.
APA
Acevedo Giraldo, D., Botero Bolívar, L., Pereira, L. T. L., Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2018). Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3799
NLM
Acevedo Giraldo D, Botero Bolívar L, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-3799
Vancouver
Acevedo Giraldo D, Botero Bolívar L, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-3799
Trabalho de evento
The influence of the boundary layer thickness on the stability of the Rossiter modes of a compressible rectangular cavity (2018)
Mathias, Marlon Sproesser ; Medeiros, Marcello Augusto Faraco de
Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidade: EESC
Subjects: AEROACÚSTICA, TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA
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ABNT
MATHIAS, Marlon Sproesser e MEDEIROS, Marcello Augusto Faraco de. The influence of the boundary layer thickness on the stability of the Rossiter modes of a compressible rectangular cavity. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3386. Acesso em: 29 nov. 2025.
APA
Mathias, M. S., & Medeiros, M. A. F. de. (2018). The influence of the boundary layer thickness on the stability of the Rossiter modes of a compressible rectangular cavity. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3386
NLM
Mathias MS, Medeiros MAF de. The influence of the boundary layer thickness on the stability of the Rossiter modes of a compressible rectangular cavity [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-3386
Vancouver
Mathias MS, Medeiros MAF de. The influence of the boundary layer thickness on the stability of the Rossiter modes of a compressible rectangular cavity [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-3386
Trabalho de evento
Experimental and numerical analysis of the aerodynamic and aeroacoustic properties of a 2D high-lift wing model (2018)
Pereira, Lourenço Tércio Lima; Botero Bolívar, Laura; Araujo, Matheus Tozo de ; Catalano, Fernando Martini ; Reis, Danillo Cafaldo dos; Coelho, Eduardo L. C
Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidades: EESC, ICMC
Subjects: AERODINÂMICA DE AERONAVES, ASAS DE AERONAVES, ANÁLISE NUMÉRICA, ENGENHARIA AERONÁUTICA
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ABNT
PEREIRA, Lourenço Tércio Lima et al. Experimental and numerical analysis of the aerodynamic and aeroacoustic properties of a 2D high-lift wing model. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3458. Acesso em: 29 nov. 2025.
APA
Pereira, L. T. L., Botero Bolívar, L., Araujo, M. T. de, Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2018). Experimental and numerical analysis of the aerodynamic and aeroacoustic properties of a 2D high-lift wing model. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3458
NLM
Pereira LTL, Botero Bolívar L, Araujo MT de, Catalano FM, Reis DC dos, Coelho ELC. Experimental and numerical analysis of the aerodynamic and aeroacoustic properties of a 2D high-lift wing model [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-3458
Vancouver
Pereira LTL, Botero Bolívar L, Araujo MT de, Catalano FM, Reis DC dos, Coelho ELC. Experimental and numerical analysis of the aerodynamic and aeroacoustic properties of a 2D high-lift wing model [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-3458
Trabalho de evento
Experimental slat noise assessment through phased array and hot-film anemometry measurements (2018)
Pereira, Lourenço Tércio Lima; Rego, Leandro Falcão Loureiro; Catalano, Fernando Martini ; Reis, Danillo Cafaldo dos; Coelho, Eduardo L. C
Source: Proceedings. Conference titles: AAIA Aerospace Sciences Meeting. Unidade: EESC
Subjects: SLATS, AEROACÚSTICA, ENGENHARIA AERONÁUTICA
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ABNT
PEREIRA, Lourenço Tércio Lima et al. Experimental slat noise assessment through phased array and hot-film anemometry measurements. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-0758. Acesso em: 29 nov. 2025.
APA
Pereira, L. T. L., Rego, L. F. L., Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2018). Experimental slat noise assessment through phased array and hot-film anemometry measurements. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-0758
NLM
Pereira LTL, Rego LFL, Catalano FM, Reis DC dos, Coelho ELC. Experimental slat noise assessment through phased array and hot-film anemometry measurements [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-0758
Vancouver
Pereira LTL, Rego LFL, Catalano FM, Reis DC dos, Coelho ELC. Experimental slat noise assessment through phased array and hot-film anemometry measurements [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-0758
Trabalho de evento
Study on a camber adaptive winglet (2018)
Eguea, João Paulo ; Catalano, Fernando Martini ; Abdalla, Alvaro Martins ; Santana, Leandro de; Venner, Cornelis H.
Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidades: EEL, EESC
Subjects: ESTRUTURA DE AERONAVES, VOO (ENGENHARIA AERONÁUTICA), ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
EGUEA, João Paulo et al. Study on a camber adaptive winglet. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3960. Acesso em: 29 nov. 2025.
APA
Eguea, J. P., Catalano, F. M., Abdalla, A. M., Santana, L. de, & Venner, C. H. (2018). Study on a camber adaptive winglet. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3960
NLM
Eguea JP, Catalano FM, Abdalla AM, Santana L de, Venner CH. Study on a camber adaptive winglet [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-3960
Vancouver
Eguea JP, Catalano FM, Abdalla AM, Santana L de, Venner CH. Study on a camber adaptive winglet [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-3960
Trabalho de evento
Noise reductions on a pusher propeller configuration through pylon tangential blowing (2018)
Rego, Leandro Falcão Loureiro; Pereira, Lourenço Tércio Lima; Catalano, Fernando Martini
Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC
Subjects: HÉLICES DE AERONAVES, AEROACÚSTICA, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
REGO, Leandro Falcão Loureiro e PEREIRA, Lourenço Tércio Lima e CATALANO, Fernando Martini. Noise reductions on a pusher propeller configuration through pylon tangential blowing. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-4194. Acesso em: 29 nov. 2025.
APA
Rego, L. F. L., Pereira, L. T. L., & Catalano, F. M. (2018). Noise reductions on a pusher propeller configuration through pylon tangential blowing. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-4194
NLM
Rego LFL, Pereira LTL, Catalano FM. Noise reductions on a pusher propeller configuration through pylon tangential blowing [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-4194
Vancouver
Rego LFL, Pereira LTL, Catalano FM. Noise reductions on a pusher propeller configuration through pylon tangential blowing [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-4194
Trabalho de evento
Aeordynamic databased of a subscale demonstrator (2017)
Jouannet, C.; Lundström, D.; Krus, P.; Sobron, A.; Silva, Roberto Gil Annes da; Catalano, Fernando Martini ; Greco Júnior, Paulo Celso
Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
JOUANNET, C. et al. Aeordynamic databased of a subscale demonstrator. 2017, Anais.. Reston, VA, USA: AIAA, 2017. Disponível em: https://repositorio.usp.br/directbitstream/38fa39ae-7494-4553-804a-d323744a4cd2/trabalho%2018%20-%20Aeordynamic%20databased%20of%20a%20subscale%20demonstrator.%20%2835th%20AIAA%20Applied%20Aerodynamics%20Conference%2C%202017%29.pdf. Acesso em: 29 nov. 2025.
APA
Jouannet, C., Lundström, D., Krus, P., Sobron, A., Silva, R. G. A. da, Catalano, F. M., & Greco Júnior, P. C. (2017). Aeordynamic databased of a subscale demonstrator. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/38fa39ae-7494-4553-804a-d323744a4cd2/trabalho%2018%20-%20Aeordynamic%20databased%20of%20a%20subscale%20demonstrator.%20%2835th%20AIAA%20Applied%20Aerodynamics%20Conference%2C%202017%29.pdf
NLM
Jouannet C, Lundström D, Krus P, Sobron A, Silva RGA da, Catalano FM, Greco Júnior PC. Aeordynamic databased of a subscale demonstrator [Internet]. Proceedings. 2017 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/38fa39ae-7494-4553-804a-d323744a4cd2/trabalho%2018%20-%20Aeordynamic%20databased%20of%20a%20subscale%20demonstrator.%20%2835th%20AIAA%20Applied%20Aerodynamics%20Conference%2C%202017%29.pdf
Vancouver
Jouannet C, Lundström D, Krus P, Sobron A, Silva RGA da, Catalano FM, Greco Júnior PC. Aeordynamic databased of a subscale demonstrator [Internet]. Proceedings. 2017 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/38fa39ae-7494-4553-804a-d323744a4cd2/trabalho%2018%20-%20Aeordynamic%20databased%20of%20a%20subscale%20demonstrator.%20%2835th%20AIAA%20Applied%20Aerodynamics%20Conference%2C%202017%29.pdf
Trabalho de evento
Baseline acoustic levels of the EESC-USP fan rig (2017)
Martínez Rocamora Junior, Bernardo; Greco Júnior, Paulo Celso ; Caldas, Luciano Coutinho; Baccalá, Luiz Antonio ; Gigena Cuenca, Rafael; Queiroz, Rudner Lauterjung
Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidades: EESC, EP
Subjects: AEROACÚSTICA, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MARTÍNEZ ROCAMORA JUNIOR, Bernardo et al. Baseline acoustic levels of the EESC-USP fan rig. 2017, Anais.. Reston, VA, USA: AIAA, 2017. Disponível em: https://repositorio.usp.br/directbitstream/db8ec149-3599-468a-b616-3e81399a078a/trabalho%2003%20-%20Baseline%20Acoustic%20Levels%20of%20the%20EESC-USP%20Fan%20Rig%20%2823rd%20AIAA-CEAS%20Aeroacoustics%20Conference%2C%202017%29.pdf. Acesso em: 29 nov. 2025.
APA
Martínez Rocamora Junior, B., Greco Júnior, P. C., Caldas, L. C., Baccalá, L. A., Gigena Cuenca, R., & Queiroz, R. L. (2017). Baseline acoustic levels of the EESC-USP fan rig. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/db8ec149-3599-468a-b616-3e81399a078a/trabalho%2003%20-%20Baseline%20Acoustic%20Levels%20of%20the%20EESC-USP%20Fan%20Rig%20%2823rd%20AIAA-CEAS%20Aeroacoustics%20Conference%2C%202017%29.pdf
NLM
Martínez Rocamora Junior B, Greco Júnior PC, Caldas LC, Baccalá LA, Gigena Cuenca R, Queiroz RL. Baseline acoustic levels of the EESC-USP fan rig [Internet]. Proceedings. 2017 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/db8ec149-3599-468a-b616-3e81399a078a/trabalho%2003%20-%20Baseline%20Acoustic%20Levels%20of%20the%20EESC-USP%20Fan%20Rig%20%2823rd%20AIAA-CEAS%20Aeroacoustics%20Conference%2C%202017%29.pdf
Vancouver
Martínez Rocamora Junior B, Greco Júnior PC, Caldas LC, Baccalá LA, Gigena Cuenca R, Queiroz RL. Baseline acoustic levels of the EESC-USP fan rig [Internet]. Proceedings. 2017 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/db8ec149-3599-468a-b616-3e81399a078a/trabalho%2003%20-%20Baseline%20Acoustic%20Levels%20of%20the%20EESC-USP%20Fan%20Rig%20%2823rd%20AIAA-CEAS%20Aeroacoustics%20Conference%2C%202017%29.pdf
Trabalho de evento
In-duct rotating beamforming and mode detection of fan noise sources (2016)
Caldas, Luciano Coutinho; Herold, Gert; Greco Júnior, Paulo Celso ; Baccalá, Luiz Antonio
Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidades: EESC, EP
Subjects: AEROACÚSTICA, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CALDAS, Luciano Coutinho et al. In-duct rotating beamforming and mode detection of fan noise sources. 2016, Anais.. Reston, VA, USA: AIAA, 2016. Disponível em: https://repositorio.usp.br/directbitstream/4acb8caf-395c-48e9-891b-42a1c246fcaa/trabalho%2007%20-%20%20In-duct%20Rotating%20Beamforming%20and%20Mode%20Detection%20of%20Fan%20Noise%20Sources%20%2822nd%20AIAACEAS%20Aeroacoustics%20Conference%202016%29%20%282%29%20%281%29_removed.pdf. Acesso em: 29 nov. 2025.
APA
Caldas, L. C., Herold, G., Greco Júnior, P. C., & Baccalá, L. A. (2016). In-duct rotating beamforming and mode detection of fan noise sources. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/4acb8caf-395c-48e9-891b-42a1c246fcaa/trabalho%2007%20-%20%20In-duct%20Rotating%20Beamforming%20and%20Mode%20Detection%20of%20Fan%20Noise%20Sources%20%2822nd%20AIAACEAS%20Aeroacoustics%20Conference%202016%29%20%282%29%20%281%29_removed.pdf
NLM
Caldas LC, Herold G, Greco Júnior PC, Baccalá LA. In-duct rotating beamforming and mode detection of fan noise sources [Internet]. Proceedings. 2016 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/4acb8caf-395c-48e9-891b-42a1c246fcaa/trabalho%2007%20-%20%20In-duct%20Rotating%20Beamforming%20and%20Mode%20Detection%20of%20Fan%20Noise%20Sources%20%2822nd%20AIAACEAS%20Aeroacoustics%20Conference%202016%29%20%282%29%20%281%29_removed.pdf
Vancouver
Caldas LC, Herold G, Greco Júnior PC, Baccalá LA. In-duct rotating beamforming and mode detection of fan noise sources [Internet]. Proceedings. 2016 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/4acb8caf-395c-48e9-891b-42a1c246fcaa/trabalho%2007%20-%20%20In-duct%20Rotating%20Beamforming%20and%20Mode%20Detection%20of%20Fan%20Noise%20Sources%20%2822nd%20AIAACEAS%20Aeroacoustics%20Conference%202016%29%20%282%29%20%281%29_removed.pdf

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