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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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: 29 nov. 2025.
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 2025 nov. 29 ] 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 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2015-1423
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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: 29 nov. 2025.
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 2025 nov. 29 ] 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 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2015-3166
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PUSTELNIK, Marcelo e SANTOS, Luis Carlos de Castro e FERRARI, Denise Beatriz. A robustness study for a D-bay grid generation criteria using surrogate models. 2014, Anais.. Reston: AIAA, 2014. Disponível em: https://doi.org/10.2514/6.2014-3238. Acesso em: 29 nov. 2025.
APA
Pustelnik, M., Santos, L. C. de C., & Ferrari, D. B. (2014). A robustness study for a D-bay grid generation criteria using surrogate models. In Proceedings. Reston: AIAA. doi:10.2514/6.2014-3238
NLM
Pustelnik M, Santos LC de C, Ferrari DB. A robustness study for a D-bay grid generation criteria using surrogate models [Internet]. Proceedings. 2014 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2014-3238
Vancouver
Pustelnik M, Santos LC de C, Ferrari DB. A robustness study for a D-bay grid generation criteria using surrogate models [Internet]. Proceedings. 2014 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2014-3238
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DIAS, José Augusto de Carvalho e DE MARQUI JÚNIOR, Carlos e ERTURK, Alper. Dimensionless analysis and scaling of a hybrid 3DOF airfoilbased piezoelectric-inductive aeroelastic energy harvester. 2013, Anais.. Reston, VA: AIAA, 2013. Disponível em: https://repositorio.usp.br/directbitstream/db8e9f0f-d1ee-4e22-98f6-11ba03e33e5e/trabalho%2021%20-%20%20Dimensionless%20analysis%20and%20scaling%20of%20a%20hybrid%203DOF%20airfoil-based%20piezoelectric-inductive%20aeroelastic%20energy%20harvester.%20%2854th%20AIAA-ASME-ASCE-AHS-ASC%20Structures%2C%20Structural%20Dynamics%2C%20and%20Materials%20C.pdf. Acesso em: 29 nov. 2025.
APA
Dias, J. A. de C., De Marqui Júnior, C., & Erturk, A. (2013). Dimensionless analysis and scaling of a hybrid 3DOF airfoilbased piezoelectric-inductive aeroelastic energy harvester. In Proceedings. Reston, VA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/db8e9f0f-d1ee-4e22-98f6-11ba03e33e5e/trabalho%2021%20-%20%20Dimensionless%20analysis%20and%20scaling%20of%20a%20hybrid%203DOF%20airfoil-based%20piezoelectric-inductive%20aeroelastic%20energy%20harvester.%20%2854th%20AIAA-ASME-ASCE-AHS-ASC%20Structures%2C%20Structural%20Dynamics%2C%20and%20Materials%20C.pdf
NLM
Dias JA de C, De Marqui Júnior C, Erturk A. Dimensionless analysis and scaling of a hybrid 3DOF airfoilbased piezoelectric-inductive aeroelastic energy harvester [Internet]. Proceedings. 2013 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/db8e9f0f-d1ee-4e22-98f6-11ba03e33e5e/trabalho%2021%20-%20%20Dimensionless%20analysis%20and%20scaling%20of%20a%20hybrid%203DOF%20airfoil-based%20piezoelectric-inductive%20aeroelastic%20energy%20harvester.%20%2854th%20AIAA-ASME-ASCE-AHS-ASC%20Structures%2C%20Structural%20Dynamics%2C%20and%20Materials%20C.pdf
Vancouver
Dias JA de C, De Marqui Júnior C, Erturk A. Dimensionless analysis and scaling of a hybrid 3DOF airfoilbased piezoelectric-inductive aeroelastic energy harvester [Internet]. Proceedings. 2013 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/db8e9f0f-d1ee-4e22-98f6-11ba03e33e5e/trabalho%2021%20-%20%20Dimensionless%20analysis%20and%20scaling%20of%20a%20hybrid%203DOF%20airfoil-based%20piezoelectric-inductive%20aeroelastic%20energy%20harvester.%20%2854th%20AIAA-ASME-ASCE-AHS-ASC%20Structures%2C%20Structural%20Dynamics%2C%20and%20Materials%20C.pdf
