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Artigo de periodico
Development of a numerical and analytical methodology for analyzing hybrid laminates with multi-oriented piezoelectric and structural layers (2024)
Longo, Janice; Silva, Matheus Rodrigues; Santana, Humberto Brito; Ferreira, Antonio Joaquim Mendes; Tita, Volnei ; Medeiros, Ricardo de
Source: Composite Structures. Unidade: EESC
Subjects: PIEZOELETRICIDADE, MÉTODO DOS ELEMENTOS FINITOS, ATUADORES PIEZELÉTRICOS, ENGENHARIA AERONÁUTICA
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ABNT
LONGO, Janice et al. Development of a numerical and analytical methodology for analyzing hybrid laminates with multi-oriented piezoelectric and structural layers. Composite Structures, v. 349-350, p. 1-9, 2024Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2024.118506. Acesso em: 06 out. 2024.
APA
Longo, J., Silva, M. R., Santana, H. B., Ferreira, A. J. M., Tita, V., & Medeiros, R. de. (2024). Development of a numerical and analytical methodology for analyzing hybrid laminates with multi-oriented piezoelectric and structural layers. Composite Structures, 349-350, 1-9. doi:10.1016/j.compstruct.2024.118506
NLM
Longo J, Silva MR, Santana HB, Ferreira AJM, Tita V, Medeiros R de. Development of a numerical and analytical methodology for analyzing hybrid laminates with multi-oriented piezoelectric and structural layers [Internet]. Composite Structures. 2024 ; 349-350 1-9.[citado 2024 out. 06 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118506
Vancouver
Longo J, Silva MR, Santana HB, Ferreira AJM, Tita V, Medeiros R de. Development of a numerical and analytical methodology for analyzing hybrid laminates with multi-oriented piezoelectric and structural layers [Internet]. Composite Structures. 2024 ; 349-350 1-9.[citado 2024 out. 06 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118506
Artigo de periodico
A nonlinear finite element analysis of laminated shells with a damage model (2024)
Santana, Pedro Bührer; Ferreira, A. J. M.; Gomes, Herbert Martins; Tita, Volnei
Source: Composites Part C: Open Access. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, DANO, ANÁLISE NÃO LINEAR DE ESTRUTURAS, ENGENHARIA AERONÁUTICA
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ABNT
SANTANA, Pedro Bührer et al. A nonlinear finite element analysis of laminated shells with a damage model. Composites Part C: Open Access, v. 15, p. 1-14, 2024Tradução . . Disponível em: http://dx.doi.org/10.1016/j.jcomc.2024.100505. Acesso em: 06 out. 2024.
APA
Santana, P. B., Ferreira, A. J. M., Gomes, H. M., & Tita, V. (2024). A nonlinear finite element analysis of laminated shells with a damage model. Composites Part C: Open Access, 15, 1-14. doi:10.1016/j.jcomc.2024.100505
NLM
Santana PB, Ferreira AJM, Gomes HM, Tita V. A nonlinear finite element analysis of laminated shells with a damage model [Internet]. Composites Part C: Open Access. 2024 ; 15 1-14.[citado 2024 out. 06 ] Available from: http://dx.doi.org/10.1016/j.jcomc.2024.100505
Vancouver
Santana PB, Ferreira AJM, Gomes HM, Tita V. A nonlinear finite element analysis of laminated shells with a damage model [Internet]. Composites Part C: Open Access. 2024 ; 15 1-14.[citado 2024 out. 06 ] Available from: http://dx.doi.org/10.1016/j.jcomc.2024.100505
Artigo de periodico
Multiscale modelling of composite laminates with voids through the direct FE2 method (2024)
Christoff, Bruno Guilherme; Almeida Júnior, José Humberto Santos; Ribeiro, Marcelo Leite ; Maciel, Maísa Milanez Ávila Dias; Guedes, Rui Miranda; Tita, Volnei
Source: Theoretical and Applied Fracture Mechanics. Unidade: EESC
Subjects: LAMINADOS, MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA AERONÁUTICA
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ABNT
CHRISTOFF, Bruno Guilherme et al. Multiscale modelling of composite laminates with voids through the direct FE2 method. Theoretical and Applied Fracture Mechanics, v. 131, p. 1-14, 2024Tradução . . Disponível em: https://dx.doi.org/10.1016/j.tafmec.2024.104424. Acesso em: 06 out. 2024.
APA
Christoff, B. G., Almeida Júnior, J. H. S., Ribeiro, M. L., Maciel, M. M. Á. D., Guedes, R. M., & Tita, V. (2024). Multiscale modelling of composite laminates with voids through the direct FE2 method. Theoretical and Applied Fracture Mechanics, 131, 1-14. doi:10.1016/j.tafmec.2024.104424
NLM
Christoff BG, Almeida Júnior JHS, Ribeiro ML, Maciel MMÁD, Guedes RM, Tita V. Multiscale modelling of composite laminates with voids through the direct FE2 method [Internet]. Theoretical and Applied Fracture Mechanics. 2024 ; 131 1-14.[citado 2024 out. 06 ] Available from: https://dx.doi.org/10.1016/j.tafmec.2024.104424
Vancouver
Christoff BG, Almeida Júnior JHS, Ribeiro ML, Maciel MMÁD, Guedes RM, Tita V. Multiscale modelling of composite laminates with voids through the direct FE2 method [Internet]. Theoretical and Applied Fracture Mechanics. 2024 ; 131 1-14.[citado 2024 out. 06 ] Available from: https://dx.doi.org/10.1016/j.tafmec.2024.104424
Artigo de periodico
Nonlinear finite element damage analysis of laminated shells by Carrera Unified Formulation (2024)
Santana, Pedro Bührer; Ferreira, Antonio Joaquim Mendes; Gomes, Herbert Martins; Tita, Volnei
Source: Composite Structures. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, ANÁLISE NÃO LINEAR DE ESTRUTURAS, DANO, ENGENHARIA AERONÁUTICA
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ABNT
SANTANA, Pedro Bührer et al. Nonlinear finite element damage analysis of laminated shells by Carrera Unified Formulation. Composite Structures, v. 348, p. 1-16, 2024Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2024.118506. Acesso em: 06 out. 2024.
APA
Santana, P. B., Ferreira, A. J. M., Gomes, H. M., & Tita, V. (2024). Nonlinear finite element damage analysis of laminated shells by Carrera Unified Formulation. Composite Structures, 348, 1-16. doi:10.1016/j.compstruct.2024.118494
NLM
Santana PB, Ferreira AJM, Gomes HM, Tita V. Nonlinear finite element damage analysis of laminated shells by Carrera Unified Formulation [Internet]. Composite Structures. 2024 ; 348 1-16.[citado 2024 out. 06 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118506
Vancouver
Santana PB, Ferreira AJM, Gomes HM, Tita V. Nonlinear finite element damage analysis of laminated shells by Carrera Unified Formulation [Internet]. Composite Structures. 2024 ; 348 1-16.[citado 2024 out. 06 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118506
Artigo de periodico
A multiobjective optimization framework for strength and stress concentration in variable axial composite shells: a metaheuristic approach (2023)
Santana, Pedro Bührer; Gomes, Herbert Martins; Ferreira, António Mendes; Tita, Volnei
Source: Latin American Journal of Solids and Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS, ESTRUTURAS
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ABNT
SANTANA, Pedro Bührer et al. A multiobjective optimization framework for strength and stress concentration in variable axial composite shells: a metaheuristic approach. Latin American Journal of Solids and Structures, v. 20, n. 6, p. 1-16, 2023Tradução . . Disponível em: http://dx.doi.org/10.1590/1679-78257577. Acesso em: 06 out. 2024.
APA
Santana, P. B., Gomes, H. M., Ferreira, A. M., & Tita, V. (2023). A multiobjective optimization framework for strength and stress concentration in variable axial composite shells: a metaheuristic approach. Latin American Journal of Solids and Structures, 20( 6), 1-16. doi:10.1590/1679-78257577
NLM
Santana PB, Gomes HM, Ferreira AM, Tita V. A multiobjective optimization framework for strength and stress concentration in variable axial composite shells: a metaheuristic approach [Internet]. Latin American Journal of Solids and Structures. 2023 ; 20( 6): 1-16.[citado 2024 out. 06 ] Available from: http://dx.doi.org/10.1590/1679-78257577
Vancouver
Santana PB, Gomes HM, Ferreira AM, Tita V. A multiobjective optimization framework for strength and stress concentration in variable axial composite shells: a metaheuristic approach [Internet]. Latin American Journal of Solids and Structures. 2023 ; 20( 6): 1-16.[citado 2024 out. 06 ] Available from: http://dx.doi.org/10.1590/1679-78257577
Trabalho de evento
Computational analysis of 2D-DCB bonded composite joints using trapezoidal traction separation law (2023)
Silva, Jailton A. P. da; Beck, Rafael; Silva, Lucas F. M. da; Tita, Volnei ; Medeiros, Ricardo de
Conference titles: Ibero-American Conference on Composite Materials - IAMaC. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, MATERIAIS COMPÓSITOS, ENGENHARIA AERONÁUTICA
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ABNT
SILVA, Jailton A. P. da et al. Computational analysis of 2D-DCB bonded composite joints using trapezoidal traction separation law. 2023, Anais.. São Carlos, SP: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2023. Disponível em: https://www.eesc.usp.br/biblioteca-admin/wp-content/uploads/2023/11/iamac2023proceedings.pdf. Acesso em: 06 out. 2024.
APA
Silva, J. A. P. da, Beck, R., Silva, L. F. M. da, Tita, V., & Medeiros, R. de. (2023). Computational analysis of 2D-DCB bonded composite joints using trapezoidal traction separation law. In . São Carlos, SP: Escola de Engenharia de São Carlos, Universidade de São Paulo. Recuperado de https://www.eesc.usp.br/biblioteca-admin/wp-content/uploads/2023/11/iamac2023proceedings.pdf
NLM
Silva JAP da, Beck R, Silva LFM da, Tita V, Medeiros R de. Computational analysis of 2D-DCB bonded composite joints using trapezoidal traction separation law [Internet]. 2023 ;[citado 2024 out. 06 ] Available from: https://www.eesc.usp.br/biblioteca-admin/wp-content/uploads/2023/11/iamac2023proceedings.pdf
Vancouver
Silva JAP da, Beck R, Silva LFM da, Tita V, Medeiros R de. Computational analysis of 2D-DCB bonded composite joints using trapezoidal traction separation law [Internet]. 2023 ;[citado 2024 out. 06 ] Available from: https://www.eesc.usp.br/biblioteca-admin/wp-content/uploads/2023/11/iamac2023proceedings.pdf
Artigo de periodico
Multiscale analysis for predicting the constitutive tensor effective coefficients of layered composites with micro and macro failures (2019)
Santana, Humberto Brito; Thiesen, Jose Luís Medeiros; Medeiros, Ricardo de; Ferreira, Antonio Joaquim Mendes; Rodríguez Ramos, Reinaldo; Tita, Volnei
Source: Applied Mathematical Modelling. Unidade: EESC
Subjects: HOMOGENEIZAÇÃO, MÉTODO DOS ELEMENTOS FINITOS
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ABNT
SANTANA, Humberto Brito et al. Multiscale analysis for predicting the constitutive tensor effective coefficients of layered composites with micro and macro failures. Applied Mathematical Modelling, v. 75, p. 250-266, 2019Tradução . . Disponível em: https://doi.org/10.1016/j.apm.2019.05.031. Acesso em: 06 out. 2024.
APA
Santana, H. B., Thiesen, J. L. M., Medeiros, R. de, Ferreira, A. J. M., Rodríguez Ramos, R., & Tita, V. (2019). Multiscale analysis for predicting the constitutive tensor effective coefficients of layered composites with micro and macro failures. Applied Mathematical Modelling, 75, 250-266. doi:10.1016/j.apm.2019.05.031
NLM
Santana HB, Thiesen JLM, Medeiros R de, Ferreira AJM, Rodríguez Ramos R, Tita V. Multiscale analysis for predicting the constitutive tensor effective coefficients of layered composites with micro and macro failures [Internet]. Applied Mathematical Modelling. 2019 ; 75 250-266.[citado 2024 out. 06 ] Available from: https://doi.org/10.1016/j.apm.2019.05.031
Vancouver
Santana HB, Thiesen JLM, Medeiros R de, Ferreira AJM, Rodríguez Ramos R, Tita V. Multiscale analysis for predicting the constitutive tensor effective coefficients of layered composites with micro and macro failures [Internet]. Applied Mathematical Modelling. 2019 ; 75 250-266.[citado 2024 out. 06 ] Available from: https://doi.org/10.1016/j.apm.2019.05.031
Trabalho de evento-anais periodico
Computational analyses of composite plates under low-velocity impact loading (2019)
Ferreira, Gregório Felipe Oliveira; Ribeiro, Marcelo Leite ; Ferreira, Antonio Joaquim Mendes; Tita, Volnei
Source: Materials Today: Proceedings. Conference titles: Brazilian Conference on Composite Materials - BCCM. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS, FALHA, ENGENHARIA AERONÁUTICA
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ABNT
FERREIRA, Gregório Felipe Oliveira et al. Computational analyses of composite plates under low-velocity impact loading. Materials Today: Proceedings. Amsterdam, Netherlands: Elsevier BV. Disponível em: https://doi.org/10.1016/j.matpr.2019.02.020. Acesso em: 06 out. 2024. , 2019
APA
Ferreira, G. F. O., Ribeiro, M. L., Ferreira, A. J. M., & Tita, V. (2019). Computational analyses of composite plates under low-velocity impact loading. Materials Today: Proceedings. Amsterdam, Netherlands: Elsevier BV. doi:10.1016/j.matpr.2019.02.020
NLM
Ferreira GFO, Ribeiro ML, Ferreira AJM, Tita V. Computational analyses of composite plates under low-velocity impact loading [Internet]. Materials Today: Proceedings. 2019 ; 8 778-788.[citado 2024 out. 06 ] Available from: https://doi.org/10.1016/j.matpr.2019.02.020
Vancouver
Ferreira GFO, Ribeiro ML, Ferreira AJM, Tita V. Computational analyses of composite plates under low-velocity impact loading [Internet]. Materials Today: Proceedings. 2019 ; 8 778-788.[citado 2024 out. 06 ] Available from: https://doi.org/10.1016/j.matpr.2019.02.020
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
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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: 06 out. 2024.
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 2024 out. 06 ] 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 2024 out. 06 ] 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
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
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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: 06 out. 2024.
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 2024 out. 06 ] 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 2024 out. 06 ] Available from: https://doi.org/10.1016/j.compstruct.2018.05.085
Artigo de periodico
Effective elastic properties of layered composites considering non-uniform imperfect adhesion (2018)
Santana, Humberto Brito; Medeiros, Ricardo de; Ferreira, Antonio Joaquim Mendes; Rodríguez Ramos, Reinaldo; Tita, Volnei
Source: Applied Mathematical Modelling. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA AERONÁUTICA
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ABNT
SANTANA, Humberto Brito et al. Effective elastic properties of layered composites considering non-uniform imperfect adhesion. Applied Mathematical Modelling, v. 59, p. 183-204, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.apm.2018.01.009. Acesso em: 06 out. 2024.
APA
Santana, H. B., Medeiros, R. de, Ferreira, A. J. M., Rodríguez Ramos, R., & Tita, V. (2018). Effective elastic properties of layered composites considering non-uniform imperfect adhesion. Applied Mathematical Modelling, 59, 183-204. doi:10.1016/j.apm.2018.01.009
NLM
Santana HB, Medeiros R de, Ferreira AJM, Rodríguez Ramos R, Tita V. Effective elastic properties of layered composites considering non-uniform imperfect adhesion [Internet]. Applied Mathematical Modelling. 2018 ; 59 183-204.[citado 2024 out. 06 ] Available from: https://doi.org/10.1016/j.apm.2018.01.009
Vancouver
Santana HB, Medeiros R de, Ferreira AJM, Rodríguez Ramos R, Tita V. Effective elastic properties of layered composites considering non-uniform imperfect adhesion [Internet]. Applied Mathematical Modelling. 2018 ; 59 183-204.[citado 2024 out. 06 ] Available from: https://doi.org/10.1016/j.apm.2018.01.009
Artigo de periodico
Finite element analysis of fluttering plates reinforced by flexible beams: an energy-based approach (2018)
Pacheco, Douglas Ramalho Queiroz; Marques, Flavio Donizeti ; Ferreira, Antonio Joaquim Mendes
Source: Journal of Sound and Vibration. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA MECÂNICA
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ABNT
PACHECO, Douglas Ramalho Queiroz e MARQUES, Flavio Donizeti e FERREIRA, Antonio Joaquim Mendes. Finite element analysis of fluttering plates reinforced by flexible beams: an energy-based approach. Journal of Sound and Vibration, v. 435, p. 135-148, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.jsv.2018.07.042. Acesso em: 06 out. 2024.
APA
Pacheco, D. R. Q., Marques, F. D., & Ferreira, A. J. M. (2018). Finite element analysis of fluttering plates reinforced by flexible beams: an energy-based approach. Journal of Sound and Vibration, 435, 135-148. doi:10.1016/j.jsv.2018.07.042
NLM
Pacheco DRQ, Marques FD, Ferreira AJM. Finite element analysis of fluttering plates reinforced by flexible beams: an energy-based approach [Internet]. Journal of Sound and Vibration. 2018 ; 435 135-148.[citado 2024 out. 06 ] Available from: https://doi.org/10.1016/j.jsv.2018.07.042
Vancouver
Pacheco DRQ, Marques FD, Ferreira AJM. Finite element analysis of fluttering plates reinforced by flexible beams: an energy-based approach [Internet]. Journal of Sound and Vibration. 2018 ; 435 135-148.[citado 2024 out. 06 ] Available from: https://doi.org/10.1016/j.jsv.2018.07.042
Trabalho de evento
The use of legendre polynomials on plate theories (2017)
Caliri Jr., Mauricio F.; Ferreira, Antonio J. M.; Tita, Volnei
Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2015. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, ESTRUTURA DE AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
CALIRI JR., Mauricio F. e FERREIRA, Antonio J. M. e TITA, Volnei. The use of legendre polynomials on plate theories. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/319/257. Acesso em: 06 out. 2024.
APA
Caliri Jr., M. F., Ferreira, A. J. M., & Tita, V. (2017). The use of legendre polynomials on plate theories. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms/paper/view/319/257
NLM
Caliri Jr. MF, Ferreira AJM, Tita V. The use of legendre polynomials on plate theories [Internet]. Anais. 2017 ;[citado 2024 out. 06 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/319/257
Vancouver
Caliri Jr. MF, Ferreira AJM, Tita V. The use of legendre polynomials on plate theories [Internet]. Anais. 2017 ;[citado 2024 out. 06 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/319/257
Artigo de periodico
Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime (2017)
Pacheco, D. R. Q.; Marques, Flavio Donizeti ; Natarajan, S.; Ferreira, A. J. M.
Source: Composite Structures. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, MÉTODO DOS ELEMENTOS FINITOS, VIBRAÇÕES DE AERONAVES, ENGENHARIA MECÂNICA
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ABNT
PACHECO, D. R. Q. et al. Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime. Composite Structures, v. 180, p. 883-891, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2017.08.058. Acesso em: 06 out. 2024.
APA
Pacheco, D. R. Q., Marques, F. D., Natarajan, S., & Ferreira, A. J. M. (2017). Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime. Composite Structures, 180, 883-891. doi:10.1016/j.compstruct.2017.08.058
NLM
Pacheco DRQ, Marques FD, Natarajan S, Ferreira AJM. Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime [Internet]. Composite Structures. 2017 ; 180 883-891.[citado 2024 out. 06 ] Available from: https://doi.org/10.1016/j.compstruct.2017.08.058
Vancouver
Pacheco DRQ, Marques FD, Natarajan S, Ferreira AJM. Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime [Internet]. Composite Structures. 2017 ; 180 883-891.[citado 2024 out. 06 ] Available from: https://doi.org/10.1016/j.compstruct.2017.08.058
Artigo de periodico
Nonlinear finite element aeroelastic analysis of multibay panels in supersonic flow regime (2017)
Pacheco, D. R. Q.; Marques, Flavio Donizeti ; Ferreira, A. J. M.
Source: Thin-Walled Structures. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, MÉTODO DOS ELEMENTOS FINITOS, ESCOAMENTO, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
PACHECO, D. R. Q. e MARQUES, Flavio Donizeti e FERREIRA, A. J. M. Nonlinear finite element aeroelastic analysis of multibay panels in supersonic flow regime. Thin-Walled Structures, v. 120, p. 470-478, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.tws.2017.08.034. Acesso em: 06 out. 2024.
APA
Pacheco, D. R. Q., Marques, F. D., & Ferreira, A. J. M. (2017). Nonlinear finite element aeroelastic analysis of multibay panels in supersonic flow regime. Thin-Walled Structures, 120, 470-478. doi:10.1016/j.tws.2017.08.034
NLM
Pacheco DRQ, Marques FD, Ferreira AJM. Nonlinear finite element aeroelastic analysis of multibay panels in supersonic flow regime [Internet]. Thin-Walled Structures. 2017 ; 120 470-478.[citado 2024 out. 06 ] Available from: https://doi.org/10.1016/j.tws.2017.08.034
Vancouver
Pacheco DRQ, Marques FD, Ferreira AJM. Nonlinear finite element aeroelastic analysis of multibay panels in supersonic flow regime [Internet]. Thin-Walled Structures. 2017 ; 120 470-478.[citado 2024 out. 06 ] Available from: https://doi.org/10.1016/j.tws.2017.08.034
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: 06 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. 06 ] 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. 06 ] 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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