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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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ABNT
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: 30 set. 2024.
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 2024 set. 30 ] 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 2024 set. 30 ] 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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ABNT
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: 30 set. 2024.
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 2024 set. 30 ] 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 2024 set. 30 ] Available from: https://doi.org/10.2514/6.2019-1867
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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ABNT
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: 30 set. 2024.
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 2024 set. 30 ] 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 2024 set. 30 ] 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: 30 set. 2024.
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 2024 set. 30 ] 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 2024 set. 30 ] Available from: https://doi.org/10.2514/6.2020-0941
Trabalho de evento
Onera-type corrections into the unsteady vortex lattice method for dynamic stall representation (2019)
Santos, Carlos Renan dos; Marques, Flavio Donizeti ; Taha, H. E.
Fonte: Proceedings. Nome do evento: International Forum on Aeroelasticity and Structural Dynamics - IFASD. Unidade: EESC
Assuntos: AEROELASTICIDADE DE AERONAVES, TRELIÇAS, ASAS DE AERONAVES, ENGENHARIA MECÂNICA
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ABNT
SANTOS, Carlos Renan dos e MARQUES, Flavio Donizeti e TAHA, H. E. Onera-type corrections into the unsteady vortex lattice method for dynamic stall representation. 2019, Anais.. Savannah, Georgia, USA: IFASD, 2019. Disponível em: https://repositorio.usp.br/directbitstream/4b87ed66-354d-4ea3-9407-b13430122efb/IFASD-2019-039.pdf. Acesso em: 30 set. 2024.
APA
Santos, C. R. dos, Marques, F. D., & Taha, H. E. (2019). Onera-type corrections into the unsteady vortex lattice method for dynamic stall representation. In Proceedings. Savannah, Georgia, USA: IFASD. Recuperado de https://repositorio.usp.br/directbitstream/4b87ed66-354d-4ea3-9407-b13430122efb/IFASD-2019-039.pdf
NLM
Santos CR dos, Marques FD, Taha HE. Onera-type corrections into the unsteady vortex lattice method for dynamic stall representation [Internet]. Proceedings. 2019 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/4b87ed66-354d-4ea3-9407-b13430122efb/IFASD-2019-039.pdf
Vancouver
Santos CR dos, Marques FD, Taha HE. Onera-type corrections into the unsteady vortex lattice method for dynamic stall representation [Internet]. Proceedings. 2019 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/4b87ed66-354d-4ea3-9407-b13430122efb/IFASD-2019-039.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: 30 set. 2024.
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 2024 set. 30 ] 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 2024 set. 30 ] Available from: https://doi.org/10.2514/6.2019-0610
Trabalho de evento
Metamodel-based optimization of an energy harvester from stall-induced pitching oscillations of airfoils (2018)
Santos, Carlos Renan dos ; Silva, Maíra Martins da ; Marques, Flavio Donizeti
Fonte: Proceedings. Nome do evento: International Conference on Noise and Vibration Engineering - ISMA. Unidade: EESC
Assuntos: AEROFÓLIOS, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA
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ABNT
SANTOS, Carlos Renan dos e SILVA, Maíra Martins da e MARQUES, Flavio Donizeti. Metamodel-based optimization of an energy harvester from stall-induced pitching oscillations of airfoils. 2018, Anais.. Leuven, Belgium: KU Leuven, 2018. Disponível em: https://repositorio.usp.br/directbitstream/3bda585e-6e58-40e2-b950-b5c0889d6956/PROD_25663_SYSNO_3124029.pdf. Acesso em: 30 set. 2024.
APA
Santos, C. R. dos, Silva, M. M. da, & Marques, F. D. (2018). Metamodel-based optimization of an energy harvester from stall-induced pitching oscillations of airfoils. In Proceedings. Leuven, Belgium: KU Leuven. Recuperado de https://repositorio.usp.br/directbitstream/3bda585e-6e58-40e2-b950-b5c0889d6956/PROD_25663_SYSNO_3124029.pdf
NLM
Santos CR dos, Silva MM da, Marques FD. Metamodel-based optimization of an energy harvester from stall-induced pitching oscillations of airfoils [Internet]. Proceedings. 2018 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/3bda585e-6e58-40e2-b950-b5c0889d6956/PROD_25663_SYSNO_3124029.pdf
Vancouver
Santos CR dos, Silva MM da, Marques FD. Metamodel-based optimization of an energy harvester from stall-induced pitching oscillations of airfoils [Internet]. Proceedings. 2018 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/3bda585e-6e58-40e2-b950-b5c0889d6956/PROD_25663_SYSNO_3124029.pdf
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: 30 set. 2024.
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 2024 set. 30 ] 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 2024 set. 30 ] Available from: https://doi.org/10.2514/6.2018-0464
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: 30 set. 2024.
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 2024 set. 30 ] 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 2024 set. 30 ] Available from: https://doi.org/10.2514/6.2018-0463
Trabalho de evento
Strucutral nonlinearitties effect on aeroelastic bifurcation phenomena in airfoils (2017)
Pereira, Daniel Almeida; Santos, Carlos Renan dos ; Marques, Flavio Donizeti
Fonte: Proceedings. Nome do evento: International Symposium on Dynamic Problems of Mechanics - DINAME. Unidade: EESC
Assuntos: AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA
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ABNT
PEREIRA, Daniel Almeida e SANTOS, Carlos Renan dos e MARQUES, Flavio Donizeti. Strucutral nonlinearitties effect on aeroelastic bifurcation phenomena in airfoils. 2017, Anais.. Rio de Janeiro, RJ: ABCM, 2017. Disponível em: https://repositorio.usp.br/directbitstream/2944c4eb-e02f-4c63-968d-6fe84db91245/PROD_25662_SYSNO_3123990.pdf. Acesso em: 30 set. 2024.
APA
Pereira, D. A., Santos, C. R. dos, & Marques, F. D. (2017). Strucutral nonlinearitties effect on aeroelastic bifurcation phenomena in airfoils. In Proceedings. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/2944c4eb-e02f-4c63-968d-6fe84db91245/PROD_25662_SYSNO_3123990.pdf
NLM
Pereira DA, Santos CR dos, Marques FD. Strucutral nonlinearitties effect on aeroelastic bifurcation phenomena in airfoils [Internet]. Proceedings. 2017 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/2944c4eb-e02f-4c63-968d-6fe84db91245/PROD_25662_SYSNO_3123990.pdf
Vancouver
Pereira DA, Santos CR dos, Marques FD. Strucutral nonlinearitties effect on aeroelastic bifurcation phenomena in airfoils [Internet]. Proceedings. 2017 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/2944c4eb-e02f-4c63-968d-6fe84db91245/PROD_25662_SYSNO_3123990.pdf
Trabalho de evento
Nonlinear airfoil torsional response induced by separated flows (2015)
Pereira, Daniel Almeida; Vasconcellos, Rui Marcos Grombone de; Marques, Flavio Donizeti
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
PEREIRA, Daniel Almeida e VASCONCELLOS, Rui Marcos Grombone de e MARQUES, Flavio Donizeti. Nonlinear airfoil torsional response induced by separated flows. 2015, Anais.. Reston, VA: AIAA, 2015. Disponível em: https://doi.org/10.2514/6.2015-1423. Acesso em: 30 set. 2024.
APA
Pereira, D. A., Vasconcellos, R. M. G. de, & Marques, F. D. (2015). Nonlinear airfoil torsional response induced by separated flows. In Proceedings. Reston, VA: AIAA. doi:10.2514/6.2015-1423
NLM
Pereira DA, Vasconcellos RMG de, Marques FD. Nonlinear airfoil torsional response induced by separated flows [Internet]. Proceedings. 2015 ;[citado 2024 set. 30 ] Available from: https://doi.org/10.2514/6.2015-1423
Vancouver
Pereira DA, Vasconcellos RMG de, Marques FD. Nonlinear airfoil torsional response induced by separated flows [Internet]. Proceedings. 2015 ;[citado 2024 set. 30 ] Available from: https://doi.org/10.2514/6.2015-1423
Trabalho de evento
An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack (2015)
Zakaria, Mohamed Y.; Pereira, Daniel Almeida; Ragab, Saad; Hajj, Muhammad R; Marques, Flavio Donizeti
Fonte: Proceedings. Nome do evento: AAIA Applied Aerodynamics Conference. Unidade: EESC
Assuntos: AERODINÂMICA DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA
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ABNT
ZAKARIA, Mohamed Y. et al. An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack. 2015, Anais.. Reston, VA, USA: AIAA, 2015. Disponível em: https://doi.org/10.2514/6.2015-3166. Acesso em: 30 set. 2024.
APA
Zakaria, M. Y., Pereira, D. A., Ragab, S., Hajj, M. R., & Marques, F. D. (2015). An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2015-3166
NLM
Zakaria MY, Pereira DA, Ragab S, Hajj MR, Marques FD. An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack [Internet]. Proceedings. 2015 ;[citado 2024 set. 30 ] Available from: https://doi.org/10.2514/6.2015-3166
Vancouver
Zakaria MY, Pereira DA, Ragab S, Hajj MR, Marques FD. An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack [Internet]. Proceedings. 2015 ;[citado 2024 set. 30 ] Available from: https://doi.org/10.2514/6.2015-3166
Trabalho de evento
Influence of structural nonlinearities in stall-induced aeroelastic response of pitching airfoils (2014)
Pereira, Daniel Almeida; Vasconcellos, Rui Marcos Grombone de; Marques, Flavio Donizeti
Fonte: Proceedings. Nome do evento: International Conference on Structural Dynamics - EURODYN. Unidade: EESC
Assuntos: AEROELASTICIDADE DE AERONAVES, VIBRAÇÕES DE AERONAVES, ENGENHARIA MECÂNICA
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ABNT
PEREIRA, Daniel Almeida e VASCONCELLOS, Rui Marcos Grombone de e MARQUES, Flavio Donizeti. Influence of structural nonlinearities in stall-induced aeroelastic response of pitching airfoils. 2014, Anais.. Porto, Portugal: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2014. Disponível em: https://repositorio.usp.br/directbitstream/f8ac4f6e-af7f-4ff6-94a6-3ca03485f916/PROD_25657_SYSNO_3123954.pdf. Acesso em: 30 set. 2024.
APA
Pereira, D. A., Vasconcellos, R. M. G. de, & Marques, F. D. (2014). Influence of structural nonlinearities in stall-induced aeroelastic response of pitching airfoils. In Proceedings. Porto, Portugal: Escola de Engenharia de São Carlos, Universidade de São Paulo. Recuperado de https://repositorio.usp.br/directbitstream/f8ac4f6e-af7f-4ff6-94a6-3ca03485f916/PROD_25657_SYSNO_3123954.pdf
NLM
Pereira DA, Vasconcellos RMG de, Marques FD. Influence of structural nonlinearities in stall-induced aeroelastic response of pitching airfoils [Internet]. Proceedings. 2014 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/f8ac4f6e-af7f-4ff6-94a6-3ca03485f916/PROD_25657_SYSNO_3123954.pdf
Vancouver
Pereira DA, Vasconcellos RMG de, Marques FD. Influence of structural nonlinearities in stall-induced aeroelastic response of pitching airfoils [Internet]. Proceedings. 2014 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/f8ac4f6e-af7f-4ff6-94a6-3ca03485f916/PROD_25657_SYSNO_3123954.pdf
Trabalho de evento
Advantages of multiple-input multiple-output (MIMO) testing using low level excitation systems (2014)
Peres, M. A.; Kallmeyer, C.; Witter, M. C.; Carneiro, R; Marques, Flavio Donizeti ; Oliveira, Leopoldo Pisanelli Rodrigues de
Fonte: Proceedings. Nome do evento: International Conference on Noise and Vibration Engineering - ISMA. Unidade: EESC
Assuntos: DINÂMICA DAS ESTRUTURAS, ESTRUTURA DE AERONAVES, ENGENHARIA MECÂNICA
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ABNT
PERES, M. A. et al. Advantages of multiple-input multiple-output (MIMO) testing using low level excitation systems. 2014, Anais.. Heverlee: KU Leuven, 2014. Disponível em: https://repositorio.usp.br/directbitstream/d857d1c1-69f4-45a8-b7ba-cbe58aa604a9/OK___trabalho%2030-%20Advantages%20of%20Multiple-Input%20Multiple-Output%20%28MIMO%29%20testing%20using%20low%20level%20excitation%20systems%20%28ISMA%202014%29.pdf. Acesso em: 30 set. 2024.
APA
Peres, M. A., Kallmeyer, C., Witter, M. C., Carneiro, R., Marques, F. D., & Oliveira, L. P. R. de. (2014). Advantages of multiple-input multiple-output (MIMO) testing using low level excitation systems. In Proceedings. Heverlee: KU Leuven. Recuperado de https://repositorio.usp.br/directbitstream/d857d1c1-69f4-45a8-b7ba-cbe58aa604a9/OK___trabalho%2030-%20Advantages%20of%20Multiple-Input%20Multiple-Output%20%28MIMO%29%20testing%20using%20low%20level%20excitation%20systems%20%28ISMA%202014%29.pdf
NLM
Peres MA, Kallmeyer C, Witter MC, Carneiro R, Marques FD, Oliveira LPR de. Advantages of multiple-input multiple-output (MIMO) testing using low level excitation systems [Internet]. Proceedings. 2014 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/d857d1c1-69f4-45a8-b7ba-cbe58aa604a9/OK___trabalho%2030-%20Advantages%20of%20Multiple-Input%20Multiple-Output%20%28MIMO%29%20testing%20using%20low%20level%20excitation%20systems%20%28ISMA%202014%29.pdf
Vancouver
Peres MA, Kallmeyer C, Witter MC, Carneiro R, Marques FD, Oliveira LPR de. Advantages of multiple-input multiple-output (MIMO) testing using low level excitation systems [Internet]. Proceedings. 2014 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/d857d1c1-69f4-45a8-b7ba-cbe58aa604a9/OK___trabalho%2030-%20Advantages%20of%20Multiple-Input%20Multiple-Output%20%28MIMO%29%20testing%20using%20low%20level%20excitation%20systems%20%28ISMA%202014%29.pdf
Trabalho de evento
Piezo-fiber composite sensor design for flutter prediction (2012)
Almeida, Alexandre Simões de; Oliveira, Leopoldo Pisanelli Rodrigues de; Marques, Flávio Donizeti
Fonte: Proceedings. Nome do evento: International Conference on Noise and Vibration Engineering - ISMA. Unidade: EESC
Assuntos: PIEZOELETRICIDADE, MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS, AEROELASTICIDADE DE AERONAVES
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ABNT
ALMEIDA, Alexandre Simões de e OLIVEIRA, Leopoldo Pisanelli Rodrigues de e MARQUES, Flávio Donizeti. Piezo-fiber composite sensor design for flutter prediction. 2012, Anais.. Heverlee: KU Leuven, 2012. Disponível em: http://past.isma-isaac.be/downloads/isma2012/papers/isma2012_0293.pdf. Acesso em: 30 set. 2024.
APA
Almeida, A. S. de, Oliveira, L. P. R. de, & Marques, F. D. (2012). Piezo-fiber composite sensor design for flutter prediction. In Proceedings. Heverlee: KU Leuven. Recuperado de http://past.isma-isaac.be/downloads/isma2012/papers/isma2012_0293.pdf
NLM
Almeida AS de, Oliveira LPR de, Marques FD. Piezo-fiber composite sensor design for flutter prediction [Internet]. Proceedings. 2012 ;[citado 2024 set. 30 ] Available from: http://past.isma-isaac.be/downloads/isma2012/papers/isma2012_0293.pdf
Vancouver
Almeida AS de, Oliveira LPR de, Marques FD. Piezo-fiber composite sensor design for flutter prediction [Internet]. Proceedings. 2012 ;[citado 2024 set. 30 ] Available from: http://past.isma-isaac.be/downloads/isma2012/papers/isma2012_0293.pdf
Trabalho de evento
Control surface freeplay nonlinearity: modeling and experimental validation (2012)
Vasconcellos, Rui Marcos Grombone de; Abdelkef, Abdessattar; 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: AERODINÂMICA DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
VASCONCELLOS, Rui Marcos Grombone de et al. Control surface freeplay nonlinearity: modeling and experimental validation. 2012, Anais.. Reston, VA: AIAA, 2012. Disponível em: https://doi.org/10.2514/6.2012-1980. Acesso em: 30 set. 2024.
APA
Vasconcellos, R. M. G. de, Abdelkef, A., Marques, F. D., & Hajj, M. R. (2012). Control surface freeplay nonlinearity: modeling and experimental validation. In Proceedings. Reston, VA: AIAA. doi:10.2514/6.2012-1980
NLM
Vasconcellos RMG de, Abdelkef A, Marques FD, Hajj MR. Control surface freeplay nonlinearity: modeling and experimental validation [Internet]. Proceedings. 2012 ;[citado 2024 set. 30 ] Available from: https://doi.org/10.2514/6.2012-1980
Vancouver
Vasconcellos RMG de, Abdelkef A, Marques FD, Hajj MR. Control surface freeplay nonlinearity: modeling and experimental validation [Internet]. Proceedings. 2012 ;[citado 2024 set. 30 ] Available from: https://doi.org/10.2514/6.2012-1980
Trabalho de evento
Numerical and experimental dynamic analyses in smart composites (2012)
Medeiros, Ricardo de; Ribeiro, Marcelo Leite; Ferreira, Gregório Felipe Oliveira; Marques, Flávio Donizeti; Tita, Volnei
Fonte: Proceedings. Nome do evento: Brazilian Conference on Composite Materials - BCCM. Unidade: EESC
Assuntos: PIEZOELETRICIDADE, MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MEDEIROS, Ricardo de et al. Numerical and experimental dynamic analyses in smart composites. 2012, Anais.. [S.l: s.n], 2012. Disponível em: https://www.researchgate.net/publication/281973602. Acesso em: 30 set. 2024.
APA
Medeiros, R. de, Ribeiro, M. L., Ferreira, G. F. O., Marques, F. D., & Tita, V. (2012). Numerical and experimental dynamic analyses in smart composites. In Proceedings. [S.l: s.n]. Recuperado de https://www.researchgate.net/publication/281973602
NLM
Medeiros R de, Ribeiro ML, Ferreira GFO, Marques FD, Tita V. Numerical and experimental dynamic analyses in smart composites [Internet]. Proceedings. 2012 ;[citado 2024 set. 30 ] Available from: https://www.researchgate.net/publication/281973602
Vancouver
Medeiros R de, Ribeiro ML, Ferreira GFO, Marques FD, Tita V. Numerical and experimental dynamic analyses in smart composites [Internet]. Proceedings. 2012 ;[citado 2024 set. 30 ] Available from: https://www.researchgate.net/publication/281973602
Trabalho de evento
Analytical study of stability of wing rock models (2010)
Entz, Ricardo Maiko Uehoka; Corrêa, Luiz Guilherme Noujain; Marques, Flávio Donizeti; Catalano, Fernando Martini; Cosin, Renato
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences. Unidade: EESC
Assuntos: SISTEMAS NÃO LINEARES, MECÂNICA DE VOO
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
ENTZ, Ricardo Maiko Uehoka et al. Analytical study of stability of wing rock models. 2010, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2010. Disponível em: https://www.researchgate.net/publication/282779238. Acesso em: 30 set. 2024.
APA
Entz, R. M. U., Corrêa, L. G. N., Marques, F. D., Catalano, F. M., & Cosin, R. (2010). Analytical study of stability of wing rock models. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS. Recuperado de https://www.researchgate.net/publication/282779238
NLM
Entz RMU, Corrêa LGN, Marques FD, Catalano FM, Cosin R. Analytical study of stability of wing rock models [Internet]. Proceedings. 2010 ;[citado 2024 set. 30 ] Available from: https://www.researchgate.net/publication/282779238
Vancouver
Entz RMU, Corrêa LGN, Marques FD, Catalano FM, Cosin R. Analytical study of stability of wing rock models [Internet]. Proceedings. 2010 ;[citado 2024 set. 30 ] Available from: https://www.researchgate.net/publication/282779238
Trabalho de evento
Time series analysis and identification of a nonlinear aeroelastic section (2010)
Vasconcellos, Rui Marcos Grombone de; 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, SISTEMAS NÃO LINEARES, ANÁLISE DE SÉRIES TEMPORAIS, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
VASCONCELLOS, Rui Marcos Grombone de e MARQUES, Flavio Donizeti e HAJJ, Muhammad R. Time series analysis and identification of a nonlinear aeroelastic section. 2010, Anais.. Reston, VA: AIAA, 2010. Disponível em: https://doi.org/10.2514/6.2010-2555. Acesso em: 30 set. 2024.
APA
Vasconcellos, R. M. G. de, Marques, F. D., & Hajj, M. R. (2010). Time series analysis and identification of a nonlinear aeroelastic section. In Proceedings. Reston, VA: AIAA. doi:10.2514/6.2010-2555
NLM
Vasconcellos RMG de, Marques FD, Hajj MR. Time series analysis and identification of a nonlinear aeroelastic section [Internet]. Proceedings. 2010 ;[citado 2024 set. 30 ] Available from: https://doi.org/10.2514/6.2010-2555
Vancouver
Vasconcellos RMG de, Marques FD, Hajj MR. Time series analysis and identification of a nonlinear aeroelastic section [Internet]. Proceedings. 2010 ;[citado 2024 set. 30 ] Available from: https://doi.org/10.2514/6.2010-2555
Trabalho de evento
Neural network metamodel-based MDO for wing design considering aeroelastic constraints (2010)
Caixeta Junior, Paulo Roberto; Marques, Flavio Donizeti
Fonte: Proceedings. Nome do evento: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Unidade: EESC
Assuntos: AEROELASTICIDADE DE AERONAVES, REDES NEURAIS, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CAIXETA JUNIOR, Paulo Roberto e MARQUES, Flavio Donizeti. Neural network metamodel-based MDO for wing design considering aeroelastic constraints. 2010, Anais.. Reston, VA: AIAA, 2010. Disponível em: https://doi.org/10.2514/6.2010-2762. Acesso em: 30 set. 2024.
APA
Caixeta Junior, P. R., & Marques, F. D. (2010). Neural network metamodel-based MDO for wing design considering aeroelastic constraints. In Proceedings. Reston, VA: AIAA. doi:10.2514/6.2010-2762
NLM
Caixeta Junior PR, Marques FD. Neural network metamodel-based MDO for wing design considering aeroelastic constraints [Internet]. Proceedings. 2010 ;[citado 2024 set. 30 ] Available from: https://doi.org/10.2514/6.2010-2762
Vancouver
Caixeta Junior PR, Marques FD. Neural network metamodel-based MDO for wing design considering aeroelastic constraints [Internet]. Proceedings. 2010 ;[citado 2024 set. 30 ] Available from: https://doi.org/10.2514/6.2010-2762

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