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Trabalho de evento
Action plane fracture criterion applied to extended finite method: a framework for onset and crack propagation (2017)
Angelo, Marcus Vinícius; Ribeiro, Marcelo Leite ; Tita, Volnei
Source: Proceedings of MECSOL. Conference titles: International Symposium on Solid Mechanics - MECSOL. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, FRATURA DAS ESTRUTURAS, JUNTAS ESTRUTURAIS, ENGENHARIA AERONÁUTICA
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ABNT
ANGELO, Marcus Vinícius e RIBEIRO, Marcelo Leite e TITA, Volnei. Action plane fracture criterion applied to extended finite method: a framework for onset and crack propagation. 2017, Anais.. Joinville, SC: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2017. . Acesso em: 19 out. 2024.
APA
Angelo, M. V., Ribeiro, M. L., & Tita, V. (2017). Action plane fracture criterion applied to extended finite method: a framework for onset and crack propagation. In Proceedings of MECSOL. Joinville, SC: Escola de Engenharia de São Carlos, Universidade de São Paulo.
NLM
Angelo MV, Ribeiro ML, Tita V. Action plane fracture criterion applied to extended finite method: a framework for onset and crack propagation. Proceedings of MECSOL. 2017 ;[citado 2024 out. 19 ]
Vancouver
Angelo MV, Ribeiro ML, Tita V. Action plane fracture criterion applied to extended finite method: a framework for onset and crack propagation. Proceedings of MECSOL. 2017 ;[citado 2024 out. 19 ]
Artigo de periodico
Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage (2017)
Almeida Júnior, José Humberto Santos; Ribeiro, Marcelo Leite ; Tita, Volnei ; Amico, Sandro Campos
Source: Composite Structures. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, ALGORITMOS GENÉTICOS, MATERIAIS COMPÓSITOS, FALHA, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
ALMEIDA JÚNIOR, José Humberto Santos et al. Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage. Composite Structures, v. 178, p. 20-26, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2017.07.054. Acesso em: 19 out. 2024.
APA
Almeida Júnior, J. H. S., Ribeiro, M. L., Tita, V., & Amico, S. C. (2017). Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage. Composite Structures, 178, 20-26. doi:10.1016/j.compstruct.2017.07.054
NLM
Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage [Internet]. Composite Structures. 2017 ; 178 20-26.[citado 2024 out. 19 ] Available from: https://doi.org/10.1016/j.compstruct.2017.07.054
Vancouver
Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage [Internet]. Composite Structures. 2017 ; 178 20-26.[citado 2024 out. 19 ] Available from: https://doi.org/10.1016/j.compstruct.2017.07.054
Trabalho de evento
Failure analysis of an al 2024-t3 plate using fracture mechanics (2017)
Silva, Jailto Antonio Prado da; Aveiga, David; Ribeiro, Marcelo Leite; Leonel, Edson Denner; Ferreira, António Joaquim Mendes; Tita, Volnei
Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2017. Unidade: EESC
Subjects: MECÂNICA DA FRATURA, MÉTODO DOS ELEMENTOS FINITOS, ESTRUTURA DE AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
SILVA, Jailto Antonio Prado da et al. Failure analysis of an al 2024-t3 plate using fracture mechanics. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/827/536. Acesso em: 19 out. 2024.
APA
Silva, J. A. P. da, Aveiga, D., Ribeiro, M. L., Leonel, E. D., Ferreira, A. J. M., & Tita, V. (2017). Failure analysis of an al 2024-t3 plate using fracture mechanics. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/827/536
NLM
Silva JAP da, Aveiga D, Ribeiro ML, Leonel ED, Ferreira AJM, Tita V. Failure analysis of an al 2024-t3 plate using fracture mechanics [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/827/536
Vancouver
Silva JAP da, Aveiga D, Ribeiro ML, Leonel ED, Ferreira AJM, Tita V. Failure analysis of an al 2024-t3 plate using fracture mechanics [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/827/536
Trabalho de evento
A numerical study on the effect of PLY orientation in lamb wave propagation through carbon fiber reinforced composites (2017)
Jaramillo Bustamante, Luis Eduardo; Santana, Humberto Brito; Tita, Volnei ; Ribeiro, Marcelo Leite
Conference titles: ABCM International Congress of Mechanical Engineering - COBEM. 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
JARAMILLO BUSTAMANTE, Luis Eduardo et al. A numerical study on the effect of PLY orientation in lamb wave propagation through carbon fiber reinforced composites. 2017, Anais.. Rio de Janeiro, RJ: ABCM, 2017. Disponível em: https://repositorio.usp.br/directbitstream/4febf50a-5f12-41fe-ad14-3e356ed7204b/trabalho%2027%20-%20%20A%20NUMERICAL%20STUDY%20ON%20THE%20EFFECT%20OF%20PLY%20ORIENTATION%20IN%20LAMB%20WAVE%20PROPAGATION%20THROUGH%20CARBON%20FIBER%20REINFORCED%20COMPOSITES%20%28COBEM%202017%29_removed.pdf. Acesso em: 19 out. 2024.
APA
Jaramillo Bustamante, L. E., Santana, H. B., Tita, V., & Ribeiro, M. L. (2017). A numerical study on the effect of PLY orientation in lamb wave propagation through carbon fiber reinforced composites. In . Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/4febf50a-5f12-41fe-ad14-3e356ed7204b/trabalho%2027%20-%20%20A%20NUMERICAL%20STUDY%20ON%20THE%20EFFECT%20OF%20PLY%20ORIENTATION%20IN%20LAMB%20WAVE%20PROPAGATION%20THROUGH%20CARBON%20FIBER%20REINFORCED%20COMPOSITES%20%28COBEM%202017%29_removed.pdf
NLM
Jaramillo Bustamante LE, Santana HB, Tita V, Ribeiro ML. A numerical study on the effect of PLY orientation in lamb wave propagation through carbon fiber reinforced composites [Internet]. 2017 ;[citado 2024 out. 19 ] Available from: https://repositorio.usp.br/directbitstream/4febf50a-5f12-41fe-ad14-3e356ed7204b/trabalho%2027%20-%20%20A%20NUMERICAL%20STUDY%20ON%20THE%20EFFECT%20OF%20PLY%20ORIENTATION%20IN%20LAMB%20WAVE%20PROPAGATION%20THROUGH%20CARBON%20FIBER%20REINFORCED%20COMPOSITES%20%28COBEM%202017%29_removed.pdf
Vancouver
Jaramillo Bustamante LE, Santana HB, Tita V, Ribeiro ML. A numerical study on the effect of PLY orientation in lamb wave propagation through carbon fiber reinforced composites [Internet]. 2017 ;[citado 2024 out. 19 ] Available from: https://repositorio.usp.br/directbitstream/4febf50a-5f12-41fe-ad14-3e356ed7204b/trabalho%2027%20-%20%20A%20NUMERICAL%20STUDY%20ON%20THE%20EFFECT%20OF%20PLY%20ORIENTATION%20IN%20LAMB%20WAVE%20PROPAGATION%20THROUGH%20CARBON%20FIBER%20REINFORCED%20COMPOSITES%20%28COBEM%202017%29_removed.pdf
Artigo de periodico
Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression (2017)
Almeida Júnior, José Humberto Santos; Ribeiro, Marcelo Leite; Tita, Volnei; Amico, Sandro Campos
Source: Composite Structures. Unidade: EESC
Subjects: ANÁLISE NUMÉRICA, FALHA, MÉTODO DOS ELEMENTOS FINITOS
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ABNT
ALMEIDA JÚNIOR, José Humberto Santos et al. Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression. Composite Structures, v. 160, n. Ja 2017, p. 204-210, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2016.10.036. Acesso em: 19 out. 2024.
APA
Almeida Júnior, J. H. S., Ribeiro, M. L., Tita, V., & Amico, S. C. (2017). Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression. Composite Structures, 160( Ja 2017), 204-210. doi:10.1016/j.compstruct.2016.10.036
NLM
Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression [Internet]. Composite Structures. 2017 ; 160( Ja 2017): 204-210.[citado 2024 out. 19 ] Available from: https://doi.org/10.1016/j.compstruct.2016.10.036
Vancouver
Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression [Internet]. Composite Structures. 2017 ; 160( Ja 2017): 204-210.[citado 2024 out. 19 ] Available from: https://doi.org/10.1016/j.compstruct.2016.10.036
Trabalho de evento
Structural health monitoring of laminated composites using lamb waves: motivations and challenges (2017)
Jaramillo Bustamante, Luis Eduardo; Ribeiro, Marcelo Leite
Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC
Subjects: DANOS MECÂNICOS, MATERIAIS COMPÓSITOS, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
JARAMILLO BUSTAMANTE, Luis Eduardo e RIBEIRO, Marcelo Leite. Structural health monitoring of laminated composites using lamb waves: motivations and challenges. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://www.eventos.eesc.usp.br/index.php/SiPGEM/iisipgem/paper/view/456/381. Acesso em: 19 out. 2024.
APA
Jaramillo Bustamante, L. E., & Ribeiro, M. L. (2017). Structural health monitoring of laminated composites using lamb waves: motivations and challenges. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://www.eventos.eesc.usp.br/index.php/SiPGEM/iisipgem/paper/view/456/381
NLM
Jaramillo Bustamante LE, Ribeiro ML. Structural health monitoring of laminated composites using lamb waves: motivations and challenges [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: http://www.eventos.eesc.usp.br/index.php/SiPGEM/iisipgem/paper/view/456/381
Vancouver
Jaramillo Bustamante LE, Ribeiro ML. Structural health monitoring of laminated composites using lamb waves: motivations and challenges [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: http://www.eventos.eesc.usp.br/index.php/SiPGEM/iisipgem/paper/view/456/381
Trabalho de evento
Analysis of delamination progression on composite laminates through XFEM based on layer wise displacement theory (2017)
Santos, Matheus Vilar Mota; Satorato, Murilo; Ribeiro, Marcelo Leite
Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2017. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, LAMINADOS, MATERIAIS COMPÓSITOS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SANTOS, Matheus Vilar Mota e SATORATO, Murilo e RIBEIRO, Marcelo Leite. Analysis of delamination progression on composite laminates through XFEM based on layer wise displacement theory. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/1012/539. Acesso em: 19 out. 2024.
APA
Santos, M. V. M., Satorato, M., & Ribeiro, M. L. (2017). Analysis of delamination progression on composite laminates through XFEM based on layer wise displacement theory. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/1012/539
NLM
Santos MVM, Satorato M, Ribeiro ML. Analysis of delamination progression on composite laminates through XFEM based on layer wise displacement theory [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/1012/539
Vancouver
Santos MVM, Satorato M, Ribeiro ML. Analysis of delamination progression on composite laminates through XFEM based on layer wise displacement theory [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/1012/539
Trabalho de evento-anais periodico
Experimental and numerical analysis of single lap bonded joints: epoxy and castor oil PU-glass fibre composites (2017)
Costa, Romeu Rony Cavalcante da; Medeiros, Ricardo de; Ribeiro, Marcelo Leite ; Tita, Volnei
Source: The Journal of Adhesion. Conference titles: Luso-Brazilian Conference on Adhesion and Adhesives (CLBA2014). Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, MATERIAIS COMPÓSITOS, MAMONA, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
COSTA, Romeu Rony Cavalcante da et al. Experimental and numerical analysis of single lap bonded joints: epoxy and castor oil PU-glass fibre composites. The Journal of Adhesion. New York, NY, USA: Taylor & Francis. Disponível em: https://doi.org/10.1080/00218464.2016.1172212. Acesso em: 19 out. 2024. , 2017
APA
Costa, R. R. C. da, Medeiros, R. de, Ribeiro, M. L., & Tita, V. (2017). Experimental and numerical analysis of single lap bonded joints: epoxy and castor oil PU-glass fibre composites. The Journal of Adhesion. New York, NY, USA: Taylor & Francis. doi:10.1080/00218464.2016.1172212
NLM
Costa RRC da, Medeiros R de, Ribeiro ML, Tita V. Experimental and numerical analysis of single lap bonded joints: epoxy and castor oil PU-glass fibre composites [Internet]. The Journal of Adhesion. 2017 ;( 1-2): 77-94.[citado 2024 out. 19 ] Available from: https://doi.org/10.1080/00218464.2016.1172212
Vancouver
Costa RRC da, Medeiros R de, Ribeiro ML, Tita V. Experimental and numerical analysis of single lap bonded joints: epoxy and castor oil PU-glass fibre composites [Internet]. The Journal of Adhesion. 2017 ;( 1-2): 77-94.[citado 2024 out. 19 ] Available from: https://doi.org/10.1080/00218464.2016.1172212
Trabalho de evento
Layerwise numerical solution for deep beams (2017)
Vilar, Matheus; Sartorato, Murilo; Ribeiro, Marcelo Leite
Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC
Subjects: FEIXES, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
VILAR, Matheus e SARTORATO, Murilo e RIBEIRO, Marcelo Leite. Layerwise numerical solution for deep beams. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://www.eventos.eesc.usp.br/index.php/SiPGEM/iisipgem/paper/view/419/367. Acesso em: 19 out. 2024.
APA
Vilar, M., Sartorato, M., & Ribeiro, M. L. (2017). Layerwise numerical solution for deep beams. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://www.eventos.eesc.usp.br/index.php/SiPGEM/iisipgem/paper/view/419/367
NLM
Vilar M, Sartorato M, Ribeiro ML. Layerwise numerical solution for deep beams [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: http://www.eventos.eesc.usp.br/index.php/SiPGEM/iisipgem/paper/view/419/367
Vancouver
Vilar M, Sartorato M, Ribeiro ML. Layerwise numerical solution for deep beams [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: http://www.eventos.eesc.usp.br/index.php/SiPGEM/iisipgem/paper/view/419/367
Trabalho de evento
A one-dimensional analytical model for damage detection on composite plates using two-dimensional lamb wave propagation (2017)
Jaramillo Bustamante, Luis Eduardo; Ribeiro, Marcelo Leite
Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2017. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, DANOS MECÂNICOS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
JARAMILLO BUSTAMANTE, Luis Eduardo e RIBEIRO, Marcelo Leite. A one-dimensional analytical model for damage detection on composite plates using two-dimensional lamb wave propagation. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/807/544. Acesso em: 19 out. 2024.
APA
Jaramillo Bustamante, L. E., & Ribeiro, M. L. (2017). A one-dimensional analytical model for damage detection on composite plates using two-dimensional lamb wave propagation. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/807/544
NLM
Jaramillo Bustamante LE, Ribeiro ML. A one-dimensional analytical model for damage detection on composite plates using two-dimensional lamb wave propagation [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/807/544
Vancouver
Jaramillo Bustamante LE, Ribeiro ML. A one-dimensional analytical model for damage detection on composite plates using two-dimensional lamb wave propagation [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/807/544
Trabalho de evento
Determination of cohesive parameters for mode I and mode II fracture analyses of e-glass/epoxy composite (2017)
Aveiga, David; Ribeiro, Marcelo Leite
Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2017. Unidade: EESC
Subjects: MECÂNICA DA FRATURA, MATERIAIS COMPÓSITOS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
AVEIGA, David e RIBEIRO, Marcelo Leite. Determination of cohesive parameters for mode I and mode II fracture analyses of e-glass/epoxy composite. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/1095/542. Acesso em: 19 out. 2024.
APA
Aveiga, D., & Ribeiro, M. L. (2017). Determination of cohesive parameters for mode I and mode II fracture analyses of e-glass/epoxy composite. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/1095/542
NLM
Aveiga D, Ribeiro ML. Determination of cohesive parameters for mode I and mode II fracture analyses of e-glass/epoxy composite [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/1095/542
Vancouver
Aveiga D, Ribeiro ML. Determination of cohesive parameters for mode I and mode II fracture analyses of e-glass/epoxy composite [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/1095/542
Trabalho de evento
Experimental dynamic investigations of bio and synthetic composites for use in aircraft interior structures (2017)
Costa, Romeu R. C. da; Eloy, Felipe de S.; Medeiros, Ricardo de; Ribeiro, Marcelo Leite; Tita, Volnei
Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2015. Unidade: EESC
Subjects: ESTRUTURA DE AERONAVES, BIOMATERIAIS, MATERIAIS COMPÓSITOS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
COSTA, Romeu R. C. da et al. Experimental dynamic investigations of bio and synthetic composites for use in aircraft interior structures. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/304/246. Acesso em: 19 out. 2024.
APA
Costa, R. R. C. da, Eloy, F. de S., Medeiros, R. de, Ribeiro, M. L., & Tita, V. (2017). Experimental dynamic investigations of bio and synthetic composites for use in aircraft interior structures. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms/paper/view/304/246
NLM
Costa RRC da, Eloy F de S, Medeiros R de, Ribeiro ML, Tita V. Experimental dynamic investigations of bio and synthetic composites for use in aircraft interior structures [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/304/246
Vancouver
Costa RRC da, Eloy F de S, Medeiros R de, Ribeiro ML, Tita V. Experimental dynamic investigations of bio and synthetic composites for use in aircraft interior structures [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/304/246
Trabalho de evento
Aplicação de ensaios para a obtenção da taxa de liberação de energia modos I e II em materiais compósitos poliméricos reforçados com fibras (2017)
Garcia, Jorge David Aveiga; Silva, Jailto Antonio Prado da; Tita, Volnei ; Ribeiro, Marcelo Leite
Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS DE FIBRAS, POLÍMEROS (MATERIAIS)
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
GARCIA, Jorge David Aveiga et al. Aplicação de ensaios para a obtenção da taxa de liberação de energia modos I e II em materiais compósitos poliméricos reforçados com fibras. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: https://repositorio.usp.br/directbitstream/bfbcd473-f795-4b29-9bba-cee3c6eaa95d/trabalho%2020%20-%20APLICA%C3%87%C3%83O%20DE%20ENSAIOS%20PARA%20A%20OBTEN%C3%87%C3%83O%20DA%20TAXA%20DE%20LIBERA%C3%87%C3%83O%20DE%20ENERGIA%20MODOS%20I%20E%20II%20EM%20MATERIAIS%20COMP%C3%93SITOS%20POLIM%C3%89RICOS%20REFOR%C3%87ADOS%20COM%20FIBRAS%20%28SIPGEM%202017%29.pdf. Acesso em: 19 out. 2024.
APA
Garcia, J. D. A., Silva, J. A. P. da, Tita, V., & Ribeiro, M. L. (2017). Aplicação de ensaios para a obtenção da taxa de liberação de energia modos I e II em materiais compósitos poliméricos reforçados com fibras. In Anais. São Carlos, SP: EESC-USP. Recuperado de https://repositorio.usp.br/directbitstream/bfbcd473-f795-4b29-9bba-cee3c6eaa95d/trabalho%2020%20-%20APLICA%C3%87%C3%83O%20DE%20ENSAIOS%20PARA%20A%20OBTEN%C3%87%C3%83O%20DA%20TAXA%20DE%20LIBERA%C3%87%C3%83O%20DE%20ENERGIA%20MODOS%20I%20E%20II%20EM%20MATERIAIS%20COMP%C3%93SITOS%20POLIM%C3%89RICOS%20REFOR%C3%87ADOS%20COM%20FIBRAS%20%28SIPGEM%202017%29.pdf
NLM
Garcia JDA, Silva JAP da, Tita V, Ribeiro ML. Aplicação de ensaios para a obtenção da taxa de liberação de energia modos I e II em materiais compósitos poliméricos reforçados com fibras [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: https://repositorio.usp.br/directbitstream/bfbcd473-f795-4b29-9bba-cee3c6eaa95d/trabalho%2020%20-%20APLICA%C3%87%C3%83O%20DE%20ENSAIOS%20PARA%20A%20OBTEN%C3%87%C3%83O%20DA%20TAXA%20DE%20LIBERA%C3%87%C3%83O%20DE%20ENERGIA%20MODOS%20I%20E%20II%20EM%20MATERIAIS%20COMP%C3%93SITOS%20POLIM%C3%89RICOS%20REFOR%C3%87ADOS%20COM%20FIBRAS%20%28SIPGEM%202017%29.pdf
Vancouver
Garcia JDA, Silva JAP da, Tita V, Ribeiro ML. Aplicação de ensaios para a obtenção da taxa de liberação de energia modos I e II em materiais compósitos poliméricos reforçados com fibras [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: https://repositorio.usp.br/directbitstream/bfbcd473-f795-4b29-9bba-cee3c6eaa95d/trabalho%2020%20-%20APLICA%C3%87%C3%83O%20DE%20ENSAIOS%20PARA%20A%20OBTEN%C3%87%C3%83O%20DA%20TAXA%20DE%20LIBERA%C3%87%C3%83O%20DE%20ENERGIA%20MODOS%20I%20E%20II%20EM%20MATERIAIS%20COMP%C3%93SITOS%20POLIM%C3%89RICOS%20REFOR%C3%87ADOS%20COM%20FIBRAS%20%28SIPGEM%202017%29.pdf
Trabalho de evento
Effective elastic properties for a periodically laminated composite considering nonuniform imperfect adhesion (2017)
Santana, Humberto Brito; Jaramillo Bustamante, Luis Eduardo; Medeiros, Ricardo de; Ribeiro, Marcelo Leite ; Tita, Volnei ; Rodríguez Ramos, Reinaldo
Source: Proceedings of MECSOL. Conference titles: International Symposium on Solid Mechanics - MECSOL. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, LAMINADOS, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SANTANA, Humberto Brito et al. Effective elastic properties for a periodically laminated composite considering nonuniform imperfect adhesion. 2017, Anais.. Joinville, SC: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2017. . Acesso em: 19 out. 2024.
APA
Santana, H. B., Jaramillo Bustamante, L. E., Medeiros, R. de, Ribeiro, M. L., Tita, V., & Rodríguez Ramos, R. (2017). Effective elastic properties for a periodically laminated composite considering nonuniform imperfect adhesion. In Proceedings of MECSOL. Joinville, SC: Escola de Engenharia de São Carlos, Universidade de São Paulo.
NLM
Santana HB, Jaramillo Bustamante LE, Medeiros R de, Ribeiro ML, Tita V, Rodríguez Ramos R. Effective elastic properties for a periodically laminated composite considering nonuniform imperfect adhesion. Proceedings of MECSOL. 2017 ;[citado 2024 out. 19 ]
Vancouver
Santana HB, Jaramillo Bustamante LE, Medeiros R de, Ribeiro ML, Tita V, Rodríguez Ramos R. Effective elastic properties for a periodically laminated composite considering nonuniform imperfect adhesion. Proceedings of MECSOL. 2017 ;[citado 2024 out. 19 ]
Trabalho de evento
Comparison between mechanical properties of bio and synthetic composites for use in aircraft interior structures (2017)
Eloy, Felipe de S.; Costa, Romeu R. C. da; Medeiros, Ricardo de; Ribeiro, Marcelo Leite; Tita, Volnei
Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2015. Unidade: EESC
Subjects: BIOMATERIAIS, MATERIAIS COMPÓSITOS, ESTRUTURA DE AERONAVES, INTERIOR DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
ELOY, Felipe de S. et al. Comparison between mechanical properties of bio and synthetic composites for use in aircraft interior structures. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/330/268. Acesso em: 19 out. 2024.
APA
Eloy, F. de S., Costa, R. R. C. da, Medeiros, R. de, Ribeiro, M. L., & Tita, V. (2017). Comparison between mechanical properties of bio and synthetic composites for use in aircraft interior structures. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms/paper/view/330/268
NLM
Eloy F de S, Costa RRC da, Medeiros R de, Ribeiro ML, Tita V. Comparison between mechanical properties of bio and synthetic composites for use in aircraft interior structures [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/330/268
Vancouver
Eloy F de S, Costa RRC da, Medeiros R de, Ribeiro ML, Tita V. Comparison between mechanical properties of bio and synthetic composites for use in aircraft interior structures [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/330/268
Trabalho de evento
Influence of stacking sequence on the radial compression of filament wound composite tubes (2017)
Almeida Jr., José Humberto S.; Ribeiro, Marcelo Leite; Tita, Volnei; Amico, Sandro C.
Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2015. Unidade: EESC
Subjects: DANO, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
ALMEIDA JR., José Humberto S. et al. Influence of stacking sequence on the radial compression of filament wound composite tubes. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/318/255. Acesso em: 19 out. 2024.
APA
Almeida Jr., J. H. S., Ribeiro, M. L., Tita, V., & Amico, S. C. (2017). Influence of stacking sequence on the radial compression of filament wound composite tubes. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms/paper/view/318/255
NLM
Almeida Jr. JHS, Ribeiro ML, Tita V, Amico SC. Influence of stacking sequence on the radial compression of filament wound composite tubes [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/318/255
Vancouver
Almeida Jr. JHS, Ribeiro ML, Tita V, Amico SC. Influence of stacking sequence on the radial compression of filament wound composite tubes [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/318/255
Trabalho de evento
Strenght prediction of single lap joints: 3D cohesive zone modelling (2017)
Madureira, Fernando; Ribeiro, Marcelo Leite
Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2017. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MADUREIRA, Fernando e RIBEIRO, Marcelo Leite. Strenght prediction of single lap joints: 3D cohesive zone modelling. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/1019/541. Acesso em: 19 out. 2024.
APA
Madureira, F., & Ribeiro, M. L. (2017). Strenght prediction of single lap joints: 3D cohesive zone modelling. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/1019/541
NLM
Madureira F, Ribeiro ML. Strenght prediction of single lap joints: 3D cohesive zone modelling [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/1019/541
Vancouver
Madureira F, Ribeiro ML. Strenght prediction of single lap joints: 3D cohesive zone modelling [Internet]. Anais. 2017 ;[citado 2024 out. 19 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/1019/541
Trabalho de evento
Dynamic analysis of laminate plates via carrera unified formulation (2017)
Ribeiro, Marcelo Leite ; Sartorato, Murilo; Medeiros, Ricardo de; Ferreira, António J. M; Tita, Volnei
Conference titles: ABCM International Congress of Mechanical Engineering - COBEM. Unidade: EESC
Subjects: 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. Dynamic analysis of laminate plates via carrera unified formulation. 2017, Anais.. Rio de Janeiro, RJ: ABCM, 2017. Disponível em: https://repositorio.usp.br/directbitstream/90152b7e-c9c3-43be-b3f1-f5d53dff656c/trabalho%2026%20-%20DYNAMIC%20ANALYSIS%20OF%20LAMINATE%20PLATES%20VIA%20CARRERA%20UNIFIED%20FORMULATION%20%28COBEM%202017%29_removed.pdf. Acesso em: 19 out. 2024.
APA
Ribeiro, M. L., Sartorato, M., Medeiros, R. de, Ferreira, A. J. M., & Tita, V. (2017). Dynamic analysis of laminate plates via carrera unified formulation. In . Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/90152b7e-c9c3-43be-b3f1-f5d53dff656c/trabalho%2026%20-%20DYNAMIC%20ANALYSIS%20OF%20LAMINATE%20PLATES%20VIA%20CARRERA%20UNIFIED%20FORMULATION%20%28COBEM%202017%29_removed.pdf
NLM
Ribeiro ML, Sartorato M, Medeiros R de, Ferreira AJM, Tita V. Dynamic analysis of laminate plates via carrera unified formulation [Internet]. 2017 ;[citado 2024 out. 19 ] Available from: https://repositorio.usp.br/directbitstream/90152b7e-c9c3-43be-b3f1-f5d53dff656c/trabalho%2026%20-%20DYNAMIC%20ANALYSIS%20OF%20LAMINATE%20PLATES%20VIA%20CARRERA%20UNIFIED%20FORMULATION%20%28COBEM%202017%29_removed.pdf
Vancouver
Ribeiro ML, Sartorato M, Medeiros R de, Ferreira AJM, Tita V. Dynamic analysis of laminate plates via carrera unified formulation [Internet]. 2017 ;[citado 2024 out. 19 ] Available from: https://repositorio.usp.br/directbitstream/90152b7e-c9c3-43be-b3f1-f5d53dff656c/trabalho%2026%20-%20DYNAMIC%20ANALYSIS%20OF%20LAMINATE%20PLATES%20VIA%20CARRERA%20UNIFIED%20FORMULATION%20%28COBEM%202017%29_removed.pdf

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