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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
Fonte: Proceedings. Nome do evento: AIAA Scitech Forum. Unidade: IME
Assuntos: 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.
Fonte: Proceedings. Nome do evento: AIAA Aviation Forum. Unidade: EESC
Assuntos: 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.
Fonte: Proceedings. Nome do evento: 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
Nonlinear dynamics of fluttering multibay panels in supersonic regime (2019)
Marques, Flavio Donizeti ; Ferreira, A. J. M.
Fonte: Proceedings. Nome do evento: AIAA Scitech Forum. Unidade: EESC
Assuntos: PAINÉIS, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA
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MARQUES, Flavio Donizeti e FERREIRA, A. J. M. Nonlinear dynamics of fluttering multibay panels in supersonic regime. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-1867. Acesso em: 29 nov. 2025.
APA
Marques, F. D., & Ferreira, A. J. M. (2019). Nonlinear dynamics of fluttering multibay panels in supersonic regime. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-1867
NLM
Marques FD, Ferreira AJM. Nonlinear dynamics of fluttering multibay panels in supersonic regime [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-1867
Vancouver
Marques FD, Ferreira AJM. Nonlinear dynamics of fluttering multibay panels in supersonic regime [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-1867
Trabalho de evento
Recirculating coherent structures inside the cove of a bulb sealed slat (2019)
Himeno, Fernando Henrique Tadashi; Amaral, Filipe Ramos do; Souza, Daniel Sampaio; Rodriguez, Daniel; Medeiros, Marcello Augusto Faraco de
Fonte: Proceedings. Nome do evento: AIAA Aviation Forum. Unidade: EESC
Assuntos: AEROACÚSTICA, SLATS, ENGENHARIA AERONÁUTICA
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ABNT
HIMENO, Fernando Henrique Tadashi et al. Recirculating coherent structures inside the cove of a bulb sealed slat. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-3695. Acesso em: 29 nov. 2025.
APA
Himeno, F. H. T., Amaral, F. R. do, Souza, D. S., Rodriguez, D., & Medeiros, M. A. F. de. (2019). Recirculating coherent structures inside the cove of a bulb sealed slat. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-3695
NLM
Himeno FHT, Amaral FR do, Souza DS, Rodriguez D, Medeiros MAF de. Recirculating coherent structures inside the cove of a bulb sealed slat [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-3695
Vancouver
Himeno FHT, Amaral FR do, Souza DS, Rodriguez D, Medeiros MAF de. Recirculating coherent structures inside the cove of a bulb sealed slat [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-3695
Trabalho de evento
The South Atlantic aerial crossing of João Ribeiro de Barros in 1927 (2019)
Marques, Flavio Donizeti ; Vasconcellos, Rui Marcos Grombone de
Fonte: Proceedings. Nome do evento: AIAA Scitech Forum. Unidade: EESC
Assuntos: BIOGRAFIAS, ENGENHARIA MECÂNICA
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MARQUES, Flavio Donizeti e VASCONCELLOS, Rui Marcos Grombone de. The South Atlantic aerial crossing of João Ribeiro de Barros in 1927. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-1953. Acesso em: 29 nov. 2025.
APA
Marques, F. D., & Vasconcellos, R. M. G. de. (2019). The South Atlantic aerial crossing of João Ribeiro de Barros in 1927. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-1953
NLM
Marques FD, Vasconcellos RMG de. The South Atlantic aerial crossing of João Ribeiro de Barros in 1927 [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-1953
Vancouver
Marques FD, Vasconcellos RMG de. The South Atlantic aerial crossing of João Ribeiro de Barros in 1927 [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-1953
Trabalho de evento
Nonlinear multibay panel flutter evaluation of composite laminates with curvilinear fibers (2019)
Guimarães, Thiago A. M.; Rade, Domingos A.; Cesnik, Carlos E. S.; Marques, Flavio Donizeti
Fonte: Proceedings. Nome do evento: AIAA Scitech Forum. Unidade: EESC
Assuntos: ENGENHARIA MECÂNICA, VIBRAÇÕES DE AERONAVES, AEROELASTICIDADE DE AERONAVES, PAINÉIS
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ABNT
GUIMARÃES, Thiago A. M. et al. Nonlinear multibay panel flutter evaluation of composite laminates with curvilinear fibers. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2020-0941. Acesso em: 29 nov. 2025.
APA
Guimarães, T. A. M., Rade, D. A., Cesnik, C. E. S., & Marques, F. D. (2019). Nonlinear multibay panel flutter evaluation of composite laminates with curvilinear fibers. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2020-0941
NLM
Guimarães TAM, Rade DA, Cesnik CES, Marques FD. Nonlinear multibay panel flutter evaluation of composite laminates with curvilinear fibers [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2020-0941
Vancouver
Guimarães TAM, Rade DA, Cesnik CES, Marques FD. Nonlinear multibay panel flutter evaluation of composite laminates with curvilinear fibers [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2020-0941
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
Fonte: Proceedings. Nome do evento: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC
Assuntos: ENGENHARIA AERONÁUTICA, AEROACÚSTICA
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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
Global instability analysis of a boundary layer flow over a small cavity (2019)
Mathias, Marlon Sproesser ; Medeiros, Marcello Augusto Faraco de
Fonte: Proceedings. Nome do evento: AIAA Aviation Forum. Unidade: EESC
Assuntos: AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
MATHIAS, Marlon Sproesser e MEDEIROS, Marcello Augusto Faraco de. Global instability analysis of a boundary layer flow over a small cavity. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-3535. Acesso em: 29 nov. 2025.
APA
Mathias, M. S., & Medeiros, M. A. F. de. (2019). Global instability analysis of a boundary layer flow over a small cavity. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-3535
NLM
Mathias MS, Medeiros MAF de. Global instability analysis of a boundary layer flow over a small cavity [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-3535
Vancouver
Mathias MS, Medeiros MAF de. Global instability analysis of a boundary layer flow over a small cavity [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-3535
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
Fonte: Proceedings. Nome do evento: AIAA Propulsion and Energy Forum. Unidade: EESC
Assuntos: 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
Stall-induced oscillations of typical aeroelastic sections in low airspeeds (2019)
Santos, Carlos Renan dos; Marques, Flavio Donizeti
Fonte: Proceedings. Nome do evento: AIAA Scitech Forum. Unidade: EESC
Assuntos: AEROFÓLIOS, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA
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ABNT
SANTOS, Carlos Renan dos e MARQUES, Flavio Donizeti. Stall-induced oscillations of typical aeroelastic sections in low airspeeds. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-0610. Acesso em: 29 nov. 2025.
APA
Santos, C. R. dos, & Marques, F. D. (2019). Stall-induced oscillations of typical aeroelastic sections in low airspeeds. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-0610
NLM
Santos CR dos, Marques FD. Stall-induced oscillations of typical aeroelastic sections in low airspeeds [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-0610
Vancouver
Santos CR dos, Marques FD. Stall-induced oscillations of typical aeroelastic sections in low airspeeds [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-0610
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
Fonte: Proceedings. Nome do evento: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC
Assuntos: 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
Structural nonlinearities influence on the energy harvesting from stall-induced oscillations (2018)
Santos, Carlos Renan dos ; Marques, Flavio Donizeti ; Hajj, Muhammad R
Fonte: Proceedings. Nome do evento: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Unidade: EESC
Assuntos: AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA
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ABNT
SANTOS, Carlos Renan dos e MARQUES, Flavio Donizeti e HAJJ, Muhammad R. Structural nonlinearities influence on the energy harvesting from stall-induced oscillations. 2018, Anais.. Reston, VA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-0464. Acesso em: 29 nov. 2025.
APA
Santos, C. R. dos, Marques, F. D., & Hajj, M. R. (2018). Structural nonlinearities influence on the energy harvesting from stall-induced oscillations. In Proceedings. Reston, VA: AIAA. doi:10.2514/6.2018-0464
NLM
Santos CR dos, Marques FD, Hajj MR. Structural nonlinearities influence on the energy harvesting from stall-induced oscillations [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-0464
Vancouver
Santos CR dos, Marques FD, Hajj MR. Structural nonlinearities influence on the energy harvesting from stall-induced oscillations [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-0464
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
Fonte: Proceedings. Nome do evento: AAIA Applied Aerodynamics Conference. Unidade: EESC
Assuntos: 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
Energy harvesting from stall-induced oscillations of pitching airfoils at high-subsonic regime (2018)
Santos, Carlos Renan dos ; Marques, Flavio Donizeti
Fonte: Proceedings. Nome do evento: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Unidade: EESC
Assuntos: AEROFÓLIOS, HELICÓPTEROS, ENGENHARIA MECÂNICA
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ABNT
SANTOS, Carlos Renan dos e MARQUES, Flavio Donizeti. Energy harvesting from stall-induced oscillations of pitching airfoils at high-subsonic regime. 2018, Anais.. Reston, VA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-0463. Acesso em: 29 nov. 2025.
APA
Santos, C. R. dos, & Marques, F. D. (2018). Energy harvesting from stall-induced oscillations of pitching airfoils at high-subsonic regime. In Proceedings. Reston, VA: AIAA. doi:10.2514/6.2018-0463
NLM
Santos CR dos, Marques FD. Energy harvesting from stall-induced oscillations of pitching airfoils at high-subsonic regime [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-0463
Vancouver
Santos CR dos, Marques FD. Energy harvesting from stall-induced oscillations of pitching airfoils at high-subsonic regime [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-0463
Trabalho de evento
Low acoustic noise and turbulence (LANT) wind-tunnel at USP-EESC (2018)
Serrano Rico, Juan Carlos; Amaral, Filipe Ramos do; Bresci, Christian Salaro; Beraldo, Matheus Maia; Medeiros, Marcello Augusto Faraco de
Fonte: Proceedings. Nome do evento: AAIA Applied Aerodynamics Conference. Unidade: EESC
Assuntos: TÚNEIS DE VENTO, AEROACÚSTICA, ENGENHARIA AERONÁUTICA
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ABNT
SERRANO RICO, Juan Carlos et al. Low acoustic noise and turbulence (LANT) wind-tunnel at USP-EESC. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3960. Acesso em: 29 nov. 2025.
APA
Serrano Rico, J. C., Amaral, F. R. do, Bresci, C. S., Beraldo, M. M., & Medeiros, M. A. F. de. (2018). Low acoustic noise and turbulence (LANT) wind-tunnel at USP-EESC. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3960
NLM
Serrano Rico JC, Amaral FR do, Bresci CS, Beraldo MM, Medeiros MAF de. Low acoustic noise and turbulence (LANT) wind-tunnel at USP-EESC [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-3960
Vancouver
Serrano Rico JC, Amaral FR do, Bresci CS, Beraldo MM, Medeiros MAF de. Low acoustic noise and turbulence (LANT) wind-tunnel at USP-EESC [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-3960
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
Fonte: Proceedings. Nome do evento: AIAA/CEAS Aeroacoustics Conference. Unidades: EESC, EP
Assuntos: 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
Fonte: Proceedings. Nome do evento: AIAA/CEAS Aeroacoustics Conference. Unidades: EESC, EP
Assuntos: 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
Trabalho de evento
Direct numerical simulation of a wavepacket in a boundary layer at Mach 0.9 (2016)
Gaviria Martínez, Germán Andrés; Medeiros, Marcello Augusto Faraco de
Fonte: Proceedings. Nome do evento: AIAA Fluid Dynamics Conference & Exhibit. Unidade: EESC
Assuntos: AEROACÚSTICA, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
GAVIRIA MARTÍNEZ, Germán Andrés e MEDEIROS, Marcello Augusto Faraco de. Direct numerical simulation of a wavepacket in a boundary layer at Mach 0.9. 2016, Anais.. Reston, VA, USA: AIAA, 2016. Disponível em: https://repositorio.usp.br/directbitstream/df087384-f496-47c5-9df7-634fbd8ac6bb/trabalho%2018%20-%20Direct%20numerical%20simulation%20of%20a%20wavepacket%20in%20a%20boundary%20layer%20at%20Mach%200.9%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf. Acesso em: 29 nov. 2025.
APA
Gaviria Martínez, G. A., & Medeiros, M. A. F. de. (2016). Direct numerical simulation of a wavepacket in a boundary layer at Mach 0.9. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/df087384-f496-47c5-9df7-634fbd8ac6bb/trabalho%2018%20-%20Direct%20numerical%20simulation%20of%20a%20wavepacket%20in%20a%20boundary%20layer%20at%20Mach%200.9%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf
NLM
Gaviria Martínez GA, Medeiros MAF de. Direct numerical simulation of a wavepacket in a boundary layer at Mach 0.9 [Internet]. Proceedings. 2016 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/df087384-f496-47c5-9df7-634fbd8ac6bb/trabalho%2018%20-%20Direct%20numerical%20simulation%20of%20a%20wavepacket%20in%20a%20boundary%20layer%20at%20Mach%200.9%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf
Vancouver
Gaviria Martínez GA, Medeiros MAF de. Direct numerical simulation of a wavepacket in a boundary layer at Mach 0.9 [Internet]. Proceedings. 2016 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/df087384-f496-47c5-9df7-634fbd8ac6bb/trabalho%2018%20-%20Direct%20numerical%20simulation%20of%20a%20wavepacket%20in%20a%20boundary%20layer%20at%20Mach%200.9%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf
Trabalho de evento
Experiments on slat noise from −6◦ to 18◦ angles of attack (2016)
Amaral, Filipe Ramos do; Pagani Júnior, Carlos do Carmo; Medeiros, Marcello Augusto Faraco de
Fonte: Proceedings. Nome do evento: AIAA Fluid Dynamics Conference & Exhibit. Unidade: EESC
Assuntos: AEROACÚSTICA, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
AMARAL, Filipe Ramos do e PAGANI JÚNIOR, Carlos do Carmo e MEDEIROS, Marcello Augusto Faraco de. Experiments on slat noise from −6◦ to 18◦ angles of attack. 2016, Anais.. Reston, VA, USA: AIAA, 2016. Disponível em: https://repositorio.usp.br/directbitstream/22944961-1231-4c8b-83df-579d6d68e5df/trabalho%2019%20-%20Experiments%20on%20Slat%20Noise%20from%20-6%C2%B0%20to%2018%C2%B0%20Angles%20of%20Attack%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf. Acesso em: 29 nov. 2025.
APA
Amaral, F. R. do, Pagani Júnior, C. do C., & Medeiros, M. A. F. de. (2016). Experiments on slat noise from −6◦ to 18◦ angles of attack. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/22944961-1231-4c8b-83df-579d6d68e5df/trabalho%2019%20-%20Experiments%20on%20Slat%20Noise%20from%20-6%C2%B0%20to%2018%C2%B0%20Angles%20of%20Attack%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf
NLM
Amaral FR do, Pagani Júnior C do C, Medeiros MAF de. Experiments on slat noise from −6◦ to 18◦ angles of attack [Internet]. Proceedings. 2016 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/22944961-1231-4c8b-83df-579d6d68e5df/trabalho%2019%20-%20Experiments%20on%20Slat%20Noise%20from%20-6%C2%B0%20to%2018%C2%B0%20Angles%20of%20Attack%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf
Vancouver
Amaral FR do, Pagani Júnior C do C, Medeiros MAF de. Experiments on slat noise from −6◦ to 18◦ angles of attack [Internet]. Proceedings. 2016 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/22944961-1231-4c8b-83df-579d6d68e5df/trabalho%2019%20-%20Experiments%20on%20Slat%20Noise%20from%20-6%C2%B0%20to%2018%C2%B0%20Angles%20of%20Attack%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf

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