ReP USP - Resultado da busca

Trabalho de evento
Identificação das derivadas de estabilidade a partir de ensaios de voo de uma aeronave rádio-controlada (2018)
Porto Alegre, Gabriel Setim; Angélico, Ricardo Afonso
Source: Anais. Conference titles: Semana de Engenharia Aeronáutica. Unidade: EESC
Subjects: DINÂMICA DE VOO, AERONAVES NÃO TRIPULADAS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
PORTO ALEGRE, Gabriel Setim e ANGÉLICO, Ricardo Afonso. Identificação das derivadas de estabilidade a partir de ensaios de voo de uma aeronave rádio-controlada. 2018, Anais.. São Carlos, SP: EESC, 2018. Disponível em: http://www.eventos.eesc.usp.br/index.php/SEAERO/seaero2018/paper/view/1216/787. Acesso em: 27 nov. 2025.
APA
Porto Alegre, G. S., & Angélico, R. A. (2018). Identificação das derivadas de estabilidade a partir de ensaios de voo de uma aeronave rádio-controlada. In Anais. São Carlos, SP: EESC. Recuperado de http://www.eventos.eesc.usp.br/index.php/SEAERO/seaero2018/paper/view/1216/787
NLM
Porto Alegre GS, Angélico RA. Identificação das derivadas de estabilidade a partir de ensaios de voo de uma aeronave rádio-controlada [Internet]. Anais. 2018 ;[citado 2025 nov. 27 ] Available from: http://www.eventos.eesc.usp.br/index.php/SEAERO/seaero2018/paper/view/1216/787
Vancouver
Porto Alegre GS, Angélico RA. Identificação das derivadas de estabilidade a partir de ensaios de voo de uma aeronave rádio-controlada [Internet]. Anais. 2018 ;[citado 2025 nov. 27 ] Available from: http://www.eventos.eesc.usp.br/index.php/SEAERO/seaero2018/paper/view/1216/787
Trabalho de evento
Computational analysis for carbon-epoxy plates damaged by low-velocity impact (2018)
Ferreira, Gregório Felipe Oliveira; Ribeiro, Marcelo Leite ; Ferreira, Antonio Joaquim Mendes; Tita, Volnei
Source: Proceedings. Conference titles: Brazilian Conference on Composite Materials - BCCM. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, MATERIAIS COMPÓSITOS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
FERREIRA, Gregório Felipe Oliveira et al. Computational analysis for carbon-epoxy plates damaged by low-velocity impact. 2018, Anais.. Rio de Janeiro, RJ: PUC-RJ, 2018. Disponível em: https://repositorio.usp.br/directbitstream/8caf63c0-a832-4e07-a8fe-e17fd3bdb32d/trabalho%2013%20-%20%20Computational%20analyses%20for%20carbon-epoxy%20plates%20damaged%20by%20low-velocity%20impact%20%28BCCM%204%202018%29_removed.pdf. Acesso em: 27 nov. 2025.
APA
Ferreira, G. F. O., Ribeiro, M. L., Ferreira, A. J. M., & Tita, V. (2018). Computational analysis for carbon-epoxy plates damaged by low-velocity impact. In Proceedings. Rio de Janeiro, RJ: PUC-RJ. Recuperado de https://repositorio.usp.br/directbitstream/8caf63c0-a832-4e07-a8fe-e17fd3bdb32d/trabalho%2013%20-%20%20Computational%20analyses%20for%20carbon-epoxy%20plates%20damaged%20by%20low-velocity%20impact%20%28BCCM%204%202018%29_removed.pdf
NLM
Ferreira GFO, Ribeiro ML, Ferreira AJM, Tita V. Computational analysis for carbon-epoxy plates damaged by low-velocity impact [Internet]. Proceedings. 2018 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/8caf63c0-a832-4e07-a8fe-e17fd3bdb32d/trabalho%2013%20-%20%20Computational%20analyses%20for%20carbon-epoxy%20plates%20damaged%20by%20low-velocity%20impact%20%28BCCM%204%202018%29_removed.pdf
Vancouver
Ferreira GFO, Ribeiro ML, Ferreira AJM, Tita V. Computational analysis for carbon-epoxy plates damaged by low-velocity impact [Internet]. Proceedings. 2018 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/8caf63c0-a832-4e07-a8fe-e17fd3bdb32d/trabalho%2013%20-%20%20Computational%20analyses%20for%20carbon-epoxy%20plates%20damaged%20by%20low-velocity%20impact%20%28BCCM%204%202018%29_removed.pdf
Artigo de periodico
The use of damping based semi-active control algorithms in the mechanical smart-spring system (2018)
Vieira, Wander Gustavo Rocha; Nitzsche, Fred; De Marqui Júnior, Carlos
Source: Journal of Vibration and Acoustics. Unidade: EESC
Subjects: SISTEMAS MECÂNICOS, VIBRAÇÕES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
VIEIRA, Wander Gustavo Rocha e NITZSCHE, Fred e DE MARQUI JÚNIOR, Carlos. The use of damping based semi-active control algorithms in the mechanical smart-spring system. Journal of Vibration and Acoustics, v. 140, p. 1-11, 2018Tradução . . Disponível em: https://doi.org/10.1115/1.4038034. Acesso em: 27 nov. 2025.
APA
Vieira, W. G. R., Nitzsche, F., & De Marqui Júnior, C. (2018). The use of damping based semi-active control algorithms in the mechanical smart-spring system. Journal of Vibration and Acoustics, 140, 1-11. doi:10.1115/1.4038034
NLM
Vieira WGR, Nitzsche F, De Marqui Júnior C. The use of damping based semi-active control algorithms in the mechanical smart-spring system [Internet]. Journal of Vibration and Acoustics. 2018 ; 140 1-11.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1115/1.4038034
Vancouver
Vieira WGR, Nitzsche F, De Marqui Júnior C. The use of damping based semi-active control algorithms in the mechanical smart-spring system [Internet]. Journal of Vibration and Acoustics. 2018 ; 140 1-11.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1115/1.4038034
Trabalho de evento
Parametric investigation of EESC-USP aeroacoustic fan rig (2018)
Gigena Cuenca, Rafael; Greco Júnior, Paulo Celso ; Martínez Rocamora Junior, Bernardo
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AEROACÚSTICA, KRIGAGEM, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
GIGENA CUENCA, Rafael e GRECO JÚNIOR, Paulo Celso e MARTÍNEZ ROCAMORA JUNIOR, Bernardo. Parametric investigation of EESC-USP aeroacoustic fan rig. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/dac92081-b591-461c-b6c2-36d72d42eab6/AP8F33~1.PDF. Acesso em: 27 nov. 2025.
APA
Gigena Cuenca, R., Greco Júnior, P. C., & Martínez Rocamora Junior, B. (2018). Parametric investigation of EESC-USP aeroacoustic fan rig. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/dac92081-b591-461c-b6c2-36d72d42eab6/AP8F33~1.PDF
NLM
Gigena Cuenca R, Greco Júnior PC, Martínez Rocamora Junior B. Parametric investigation of EESC-USP aeroacoustic fan rig [Internet]. Proceedings. 2018 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/dac92081-b591-461c-b6c2-36d72d42eab6/AP8F33~1.PDF
Vancouver
Gigena Cuenca R, Greco Júnior PC, Martínez Rocamora Junior B. Parametric investigation of EESC-USP aeroacoustic fan rig [Internet]. Proceedings. 2018 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/dac92081-b591-461c-b6c2-36d72d42eab6/AP8F33~1.PDF
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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 27 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. 27 ] 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. 27 ] 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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 27 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. 27 ] 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. 27 ] Available from: https://doi.org/10.2514/6.2018-0759
Trabalho de evento
Flight dynamics modeling and trim curves of a conceptual semi-tandem wing VTOL UAV (2018)
Daud Filho, Antonio Carlos; Belo, Eduardo Morgado
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: DINÂMICA DE VOO, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
DAUD FILHO, Antonio Carlos e BELO, Eduardo Morgado. Flight dynamics modeling and trim curves of a conceptual semi-tandem wing VTOL UAV. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/987dd969-af4d-49be-a001-64ec8719b596/trabalho%2001%20-%20FLIGHT%20DYNAMICS%20MODELING%20AND%20TRIM%20CURVES%20OF%20A%20CONCEPTUAL%20SEMI-TANDEM%20WING%20VTOL%20UAV%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf. Acesso em: 27 nov. 2025.
APA
Daud Filho, A. C., & Belo, E. M. (2018). Flight dynamics modeling and trim curves of a conceptual semi-tandem wing VTOL UAV. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/987dd969-af4d-49be-a001-64ec8719b596/trabalho%2001%20-%20FLIGHT%20DYNAMICS%20MODELING%20AND%20TRIM%20CURVES%20OF%20A%20CONCEPTUAL%20SEMI-TANDEM%20WING%20VTOL%20UAV%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf
NLM
Daud Filho AC, Belo EM. Flight dynamics modeling and trim curves of a conceptual semi-tandem wing VTOL UAV [Internet]. Proceedings. 2018 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/987dd969-af4d-49be-a001-64ec8719b596/trabalho%2001%20-%20FLIGHT%20DYNAMICS%20MODELING%20AND%20TRIM%20CURVES%20OF%20A%20CONCEPTUAL%20SEMI-TANDEM%20WING%20VTOL%20UAV%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf
Vancouver
Daud Filho AC, Belo EM. Flight dynamics modeling and trim curves of a conceptual semi-tandem wing VTOL UAV [Internet]. Proceedings. 2018 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/987dd969-af4d-49be-a001-64ec8719b596/trabalho%2001%20-%20FLIGHT%20DYNAMICS%20MODELING%20AND%20TRIM%20CURVES%20OF%20A%20CONCEPTUAL%20SEMI-TANDEM%20WING%20VTOL%20UAV%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf
Artigo de periodico
A delamination propagation model for fiber reinforced laminated composite materials (2018)
Garcia, Jorge David Aveiga; Ribeiro, Marcelo Leite
Source: Mathematical Problems in Engineering. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, ESTRUTURA DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
GARCIA, Jorge David Aveiga e RIBEIRO, Marcelo Leite. A delamination propagation model for fiber reinforced laminated composite materials. Mathematical Problems in Engineering, v. 2018, p. 1-10, 2018Tradução . . Disponível em: https://doi.org/10.1155/2018/1861268. Acesso em: 27 nov. 2025.
APA
Garcia, J. D. A., & Ribeiro, M. L. (2018). A delamination propagation model for fiber reinforced laminated composite materials. Mathematical Problems in Engineering, 2018, 1-10. doi:10.1155/2018/1861268
NLM
Garcia JDA, Ribeiro ML. A delamination propagation model for fiber reinforced laminated composite materials [Internet]. Mathematical Problems in Engineering. 2018 ; 2018 1-10.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1155/2018/1861268
Vancouver
Garcia JDA, Ribeiro ML. A delamination propagation model for fiber reinforced laminated composite materials [Internet]. Mathematical Problems in Engineering. 2018 ; 2018 1-10.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1155/2018/1861268
Artigo de periodico
Multi-scale analyses of a floating marine hose with hybrid polyaramid/polyamide reinforcement cords (2018)
Tonatto, Maikson Luiz Passaia; Tita, Volnei ; Forte, Maria M. C.; Amico, Sandro C.
Source: Marine Structures. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
TONATTO, Maikson Luiz Passaia et al. Multi-scale analyses of a floating marine hose with hybrid polyaramid/polyamide reinforcement cords. Marine Structures, v. 60, p. 279-292, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.marstruc.2018.04.005. Acesso em: 27 nov. 2025.
APA
Tonatto, M. L. P., Tita, V., Forte, M. M. C., & Amico, S. C. (2018). Multi-scale analyses of a floating marine hose with hybrid polyaramid/polyamide reinforcement cords. Marine Structures, 60, 279-292. doi:10.1016/j.marstruc.2018.04.005
NLM
Tonatto MLP, Tita V, Forte MMC, Amico SC. Multi-scale analyses of a floating marine hose with hybrid polyaramid/polyamide reinforcement cords [Internet]. Marine Structures. 2018 ; 60 279-292.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.marstruc.2018.04.005
Vancouver
Tonatto MLP, Tita V, Forte MMC, Amico SC. Multi-scale analyses of a floating marine hose with hybrid polyaramid/polyamide reinforcement cords [Internet]. Marine Structures. 2018 ; 60 279-292.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.marstruc.2018.04.005
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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 27 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. 27 ] 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. 27 ] Available from: https://doi.org/10.2514/6.2018-3799
Artigo de periodico
Conceptual design and CFD analysis of a new prototype of agricultural aircraft (2018)
Bravo Mosquera, Pedro David; Cerón Muñoz, Hernán Darío ; Díaz Vázquez, Guillermo; Catalano, Fernando Martini
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, AERONAVES AGRÍCOLAS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BRAVO MOSQUERA, Pedro David et al. Conceptual design and CFD analysis of a new prototype of agricultural aircraft. Aerospace Science and Technology, v. 80, p. 156-176, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2018.07.014. Acesso em: 27 nov. 2025.
APA
Bravo Mosquera, P. D., Cerón Muñoz, H. D., Díaz Vázquez, G., & Catalano, F. M. (2018). Conceptual design and CFD analysis of a new prototype of agricultural aircraft. Aerospace Science and Technology, 80, 156-176. doi:10.1016/j.ast.2018.07.014
NLM
Bravo Mosquera PD, Cerón Muñoz HD, Díaz Vázquez G, Catalano FM. Conceptual design and CFD analysis of a new prototype of agricultural aircraft [Internet]. Aerospace Science and Technology. 2018 ; 80 156-176.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.ast.2018.07.014
Vancouver
Bravo Mosquera PD, Cerón Muñoz HD, Díaz Vázquez G, Catalano FM. Conceptual design and CFD analysis of a new prototype of agricultural aircraft [Internet]. Aerospace Science and Technology. 2018 ; 80 156-176.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.ast.2018.07.014
Artigo de periodico
On the electrode segmentation for piezoelectric energy harvesting from nonlinear limit cycle oscillations in axial flow (2018)
De Marqui Júnior, Carlos ; Tan, David; Erturk, Alper
Source: Journal of Fluids and Structures. Unidade: EESC
Subjects: ENERGIA, PIEZOELETRICIDADE, AEROELASTICIDADE DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
DE MARQUI JÚNIOR, Carlos e TAN, David e ERTURK, Alper. On the electrode segmentation for piezoelectric energy harvesting from nonlinear limit cycle oscillations in axial flow. Journal of Fluids and Structures, v. 82, p. 492-504, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.jfluidstructs.2018.07.020. Acesso em: 27 nov. 2025.
APA
De Marqui Júnior, C., Tan, D., & Erturk, A. (2018). On the electrode segmentation for piezoelectric energy harvesting from nonlinear limit cycle oscillations in axial flow. Journal of Fluids and Structures, 82, 492-504. doi:10.1016/j.jfluidstructs.2018.07.020
NLM
De Marqui Júnior C, Tan D, Erturk A. On the electrode segmentation for piezoelectric energy harvesting from nonlinear limit cycle oscillations in axial flow [Internet]. Journal of Fluids and Structures. 2018 ; 82 492-504.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.jfluidstructs.2018.07.020
Vancouver
De Marqui Júnior C, Tan D, Erturk A. On the electrode segmentation for piezoelectric energy harvesting from nonlinear limit cycle oscillations in axial flow [Internet]. Journal of Fluids and Structures. 2018 ; 82 492-504.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.jfluidstructs.2018.07.020
Artigo de periodico
Adaptive locally resonant metamaterials leveraging shape memory alloys (2018)
Sousa, Vagner Candido de; Sugino, Christopher; De Marqui Júnior, Carlos ; Erturk, Alper
Source: Journal of Applied Physics. Unidade: EESC
Subjects: VIBRAÇÕES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SOUSA, Vagner Candido de et al. Adaptive locally resonant metamaterials leveraging shape memory alloys. Journal of Applied Physics, v. 124, p. 1-11, 2018Tradução . . Disponível em: https://doi.org/10.1063/1.5031168. Acesso em: 27 nov. 2025.
APA
Sousa, V. C. de, Sugino, C., De Marqui Júnior, C., & Erturk, A. (2018). Adaptive locally resonant metamaterials leveraging shape memory alloys. Journal of Applied Physics, 124, 1-11. doi:10.1063/1.5031168
NLM
Sousa VC de, Sugino C, De Marqui Júnior C, Erturk A. Adaptive locally resonant metamaterials leveraging shape memory alloys [Internet]. Journal of Applied Physics. 2018 ; 124 1-11.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1063/1.5031168
Vancouver
Sousa VC de, Sugino C, De Marqui Júnior C, Erturk A. Adaptive locally resonant metamaterials leveraging shape memory alloys [Internet]. Journal of Applied Physics. 2018 ; 124 1-11.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1063/1.5031168
Artigo de periodico
An experimentally validated piezoelectric nonlinear energy sink for wideband vibration attenuation (2018)
Silva, Tarcísio Marinelli Pereira; Clementino, Marcel Araujo; De Marqui Júnior, Carlos ; Erturk, Alper
Source: Journal of Sound and Vibration. Unidade: EESC
Subjects: PIEZOELETRICIDADE, ENERGIA, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SILVA, Tarcísio Marinelli Pereira et al. An experimentally validated piezoelectric nonlinear energy sink for wideband vibration attenuation. Journal of Sound and Vibration, v. 437, p. 68-78, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.jsv.2018.08.038. Acesso em: 27 nov. 2025.
APA
Silva, T. M. P., Clementino, M. A., De Marqui Júnior, C., & Erturk, A. (2018). An experimentally validated piezoelectric nonlinear energy sink for wideband vibration attenuation. Journal of Sound and Vibration, 437, 68-78. doi:10.1016/j.jsv.2018.08.038
NLM
Silva TMP, Clementino MA, De Marqui Júnior C, Erturk A. An experimentally validated piezoelectric nonlinear energy sink for wideband vibration attenuation [Internet]. Journal of Sound and Vibration. 2018 ; 437 68-78.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.jsv.2018.08.038
Vancouver
Silva TMP, Clementino MA, De Marqui Júnior C, Erturk A. An experimentally validated piezoelectric nonlinear energy sink for wideband vibration attenuation [Internet]. Journal of Sound and Vibration. 2018 ; 437 68-78.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.jsv.2018.08.038
Artigo de periodico
Pilot induced oscillations adaptive suppression in fly-by-wire systems (2018)
Moura, Herlandson Cardoso de; Bidinotto, Jorge Henrique ; Belo, Eduardo Morgado
Source: International Journal of Aerospace and Mechanical Engineering. Unidade: EESC
Subjects: CONTROLE ADAPTATIVO, SIMULADORES DE VOO, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MOURA, Herlandson Cardoso de e BIDINOTTO, Jorge Henrique e BELO, Eduardo Morgado. Pilot induced oscillations adaptive suppression in fly-by-wire systems. International Journal of Aerospace and Mechanical Engineering, v. 12, n. 9, p. 870-876, 2018Tradução . . Disponível em: https://repositorio.usp.br/directbitstream/30be2ac7-00ea-4416-bff6-afa0223fe8c1/artigo%2004%20-%20Pilot%20Induced%20Oscillations%20Adaptive%20Suppression%20in%20Fly-By-Wire%20Systems%20%28International%20Journal%20of%20Aerospace%20and%20Mechanical%20Engineering%29.pdf. Acesso em: 27 nov. 2025.
APA
Moura, H. C. de, Bidinotto, J. H., & Belo, E. M. (2018). Pilot induced oscillations adaptive suppression in fly-by-wire systems. International Journal of Aerospace and Mechanical Engineering, 12( 9), 870-876. Recuperado de https://repositorio.usp.br/directbitstream/30be2ac7-00ea-4416-bff6-afa0223fe8c1/artigo%2004%20-%20Pilot%20Induced%20Oscillations%20Adaptive%20Suppression%20in%20Fly-By-Wire%20Systems%20%28International%20Journal%20of%20Aerospace%20and%20Mechanical%20Engineering%29.pdf
NLM
Moura HC de, Bidinotto JH, Belo EM. Pilot induced oscillations adaptive suppression in fly-by-wire systems [Internet]. International Journal of Aerospace and Mechanical Engineering. 2018 ; 12( 9): 870-876.[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/30be2ac7-00ea-4416-bff6-afa0223fe8c1/artigo%2004%20-%20Pilot%20Induced%20Oscillations%20Adaptive%20Suppression%20in%20Fly-By-Wire%20Systems%20%28International%20Journal%20of%20Aerospace%20and%20Mechanical%20Engineering%29.pdf
Vancouver
Moura HC de, Bidinotto JH, Belo EM. Pilot induced oscillations adaptive suppression in fly-by-wire systems [Internet]. International Journal of Aerospace and Mechanical Engineering. 2018 ; 12( 9): 870-876.[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/30be2ac7-00ea-4416-bff6-afa0223fe8c1/artigo%2004%20-%20Pilot%20Induced%20Oscillations%20Adaptive%20Suppression%20in%20Fly-By-Wire%20Systems%20%28International%20Journal%20of%20Aerospace%20and%20Mechanical%20Engineering%29.pdf
Trabalho de evento
Aerodynamic heating effect on roughness, aerodynamic coefficients and power output of aerogenerators: a discussion (2018)
Ribeiro, Daniel Garcia; Cerón Muñoz, Hernán Darío ; Bravo Mosquera, Pedro David
Source: Proceedings of ENCIT. Conference titles: Brazilian Congress of Thermal Sciences and Engineering. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, TURBINAS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
RIBEIRO, Daniel Garcia e CERÓN MUÑOZ, Hernán Darío e BRAVO MOSQUERA, Pedro David. Aerodynamic heating effect on roughness, aerodynamic coefficients and power output of aerogenerators: a discussion. 2018, Anais.. Rio de Janeiro, RJ: ABCM, 2018. Disponível em: https://repositorio.usp.br/directbitstream/715b85dc-28f5-4e9a-b32f-eb96c4d45f34/trabalho%2006%20-%20Aerodynamic%20Heating%20Effect%20on%20Roughness%2C%20Aerodynamic%20Coefficients%20and%20Power%20Output%20of%20Aerogenerators%20-%20a%20Discussion%20%2817th%20Brazilian%20Congress%20of%20Thermal%20Sciences%20and%20Engineering%202018%29_removed.pdf. Acesso em: 27 nov. 2025.
APA
Ribeiro, D. G., Cerón Muñoz, H. D., & Bravo Mosquera, P. D. (2018). Aerodynamic heating effect on roughness, aerodynamic coefficients and power output of aerogenerators: a discussion. In Proceedings of ENCIT. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/715b85dc-28f5-4e9a-b32f-eb96c4d45f34/trabalho%2006%20-%20Aerodynamic%20Heating%20Effect%20on%20Roughness%2C%20Aerodynamic%20Coefficients%20and%20Power%20Output%20of%20Aerogenerators%20-%20a%20Discussion%20%2817th%20Brazilian%20Congress%20of%20Thermal%20Sciences%20and%20Engineering%202018%29_removed.pdf
NLM
Ribeiro DG, Cerón Muñoz HD, Bravo Mosquera PD. Aerodynamic heating effect on roughness, aerodynamic coefficients and power output of aerogenerators: a discussion [Internet]. Proceedings of ENCIT. 2018 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/715b85dc-28f5-4e9a-b32f-eb96c4d45f34/trabalho%2006%20-%20Aerodynamic%20Heating%20Effect%20on%20Roughness%2C%20Aerodynamic%20Coefficients%20and%20Power%20Output%20of%20Aerogenerators%20-%20a%20Discussion%20%2817th%20Brazilian%20Congress%20of%20Thermal%20Sciences%20and%20Engineering%202018%29_removed.pdf
Vancouver
Ribeiro DG, Cerón Muñoz HD, Bravo Mosquera PD. Aerodynamic heating effect on roughness, aerodynamic coefficients and power output of aerogenerators: a discussion [Internet]. Proceedings of ENCIT. 2018 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/715b85dc-28f5-4e9a-b32f-eb96c4d45f34/trabalho%2006%20-%20Aerodynamic%20Heating%20Effect%20on%20Roughness%2C%20Aerodynamic%20Coefficients%20and%20Power%20Output%20of%20Aerogenerators%20-%20a%20Discussion%20%2817th%20Brazilian%20Congress%20of%20Thermal%20Sciences%20and%20Engineering%202018%29_removed.pdf
Trabalho de evento
Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica (2018)
Parra Peñuela, Héctor; Gómez Rivera, William; Cerón Muñoz, Hernán Darío
Source: Proceedings. Conference titles: Congreso Latinoamericano de Ingeniería Mecánica - COLIM. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, TURBINAS, ENERGIA EÓLICA, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
PARRA PEÑUELA, Héctor e GÓMEZ RIVERA, William e CERÓN MUÑOZ, Hernán Darío. Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica. 2018, Anais.. Pamplona, Colômbia: Universidad Pamplona, 2018. Disponível em: https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf. Acesso em: 27 nov. 2025.
APA
Parra Peñuela, H., Gómez Rivera, W., & Cerón Muñoz, H. D. (2018). Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica. In Proceedings. Pamplona, Colômbia: Universidad Pamplona. Recuperado de https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf
NLM
Parra Peñuela H, Gómez Rivera W, Cerón Muñoz HD. Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica [Internet]. Proceedings. 2018 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf
Vancouver
Parra Peñuela H, Gómez Rivera W, Cerón Muñoz HD. Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica [Internet]. Proceedings. 2018 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf
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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 27 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. 27 ] 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. 27 ] Available from: https://doi.org/10.2514/6.2018-3386
Artigo de periodico
A computational framework for predicting onset and crack propagation in composite structures via extended Finite Element Method (XFEM) (2018)
Angelo, Marcus Vinícius; Ribeiro, Marcelo Leite ; Tita, Volnei
Source: Latin American Journal of Solids and Structures. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, FALHA, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
ANGELO, Marcus Vinícius e RIBEIRO, Marcelo Leite e TITA, Volnei. A computational framework for predicting onset and crack propagation in composite structures via extended Finite Element Method (XFEM). Latin American Journal of Solids and Structures, v. 15, n. 11 (thematic section), p. 1-14, 2018Tradução . . Disponível em: https://doi.org/10.1590/1679-78254301. Acesso em: 27 nov. 2025.
APA
Angelo, M. V., Ribeiro, M. L., & Tita, V. (2018). A computational framework for predicting onset and crack propagation in composite structures via extended Finite Element Method (XFEM). Latin American Journal of Solids and Structures, 15( 11 (thematic section), 1-14. doi:10.1590/1679-78254301
NLM
Angelo MV, Ribeiro ML, Tita V. A computational framework for predicting onset and crack propagation in composite structures via extended Finite Element Method (XFEM) [Internet]. Latin American Journal of Solids and Structures. 2018 ; 15( 11 (thematic section): 1-14.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1590/1679-78254301
Vancouver
Angelo MV, Ribeiro ML, Tita V. A computational framework for predicting onset and crack propagation in composite structures via extended Finite Element Method (XFEM) [Internet]. Latin American Journal of Solids and Structures. 2018 ; 15( 11 (thematic section): 1-14.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1590/1679-78254301
Artigo de periodico
Experimental and numerical dynamic analysis of laminate plates via Carrera Unified Formulation (2018)
Ribeiro, Marcelo Leite ; Ferreira, Gregório Felipe Oliveira; Medeiros, Ricardo de; Ferreira, Antonio Joaquim Mendes; Tita, Volnei
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS, VIBRAÇÕES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
RIBEIRO, Marcelo Leite et al. Experimental and numerical dynamic analysis of laminate plates via Carrera Unified Formulation. Composite Structures, v. 202, p. 1176-1185, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2018.05.085. Acesso em: 27 nov. 2025.
APA
Ribeiro, M. L., Ferreira, G. F. O., Medeiros, R. de, Ferreira, A. J. M., & Tita, V. (2018). Experimental and numerical dynamic analysis of laminate plates via Carrera Unified Formulation. Composite Structures, 202, 1176-1185. doi:10.1016/j.compstruct.2018.05.085
NLM
Ribeiro ML, Ferreira GFO, Medeiros R de, Ferreira AJM, Tita V. Experimental and numerical dynamic analysis of laminate plates via Carrera Unified Formulation [Internet]. Composite Structures. 2018 ; 202 1176-1185.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.compstruct.2018.05.085
Vancouver
Ribeiro ML, Ferreira GFO, Medeiros R de, Ferreira AJM, Tita V. Experimental and numerical dynamic analysis of laminate plates via Carrera Unified Formulation [Internet]. Composite Structures. 2018 ; 202 1176-1185.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.compstruct.2018.05.085

USP Schools

ReP

Filtros

Authors

USP affiliated authors

Subjects

Source title

Publisher

Conference titles

Countries/Territories

Funding Agencies

Indexado em

Non normalized affiliation

Countries of institutions of collaboration