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Artigo de periodico
A review on bistable composite laminates for aerospace applications (2024)
Lemos, Diego Magela; Marques, Flavio Donizeti ; Ferreira, Antonio Joaquim Mendes
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, LAMINADOS, ENGENHARIA MECÂNICA
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ABNT
LEMOS, Diego Magela e MARQUES, Flavio Donizeti e FERREIRA, Antonio Joaquim Mendes. A review on bistable composite laminates for aerospace applications. Composite Structures, v. 329, p. 1-21, 2024Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2023.117756. Acesso em: 10 nov. 2025.
APA
Lemos, D. M., Marques, F. D., & Ferreira, A. J. M. (2024). A review on bistable composite laminates for aerospace applications. Composite Structures, 329, 1-21. doi:10.1016/j.compstruct.2023.117756
NLM
Lemos DM, Marques FD, Ferreira AJM. A review on bistable composite laminates for aerospace applications [Internet]. Composite Structures. 2024 ; 329 1-21.[citado 2025 nov. 10 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2023.117756
Vancouver
Lemos DM, Marques FD, Ferreira AJM. A review on bistable composite laminates for aerospace applications [Internet]. Composite Structures. 2024 ; 329 1-21.[citado 2025 nov. 10 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2023.117756
Artigo de periodico
Crashworthiness assessment of a composite fuselage stanchion employing a strain rate dependent damage model (2024)
Miranda, Mario; Cini, Andrea; Raimondo, Antonio; Tita, Volnei
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, FUSELAGEM DE AERONAVES, DANO, ESTRUTURA DE AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
MIRANDA, Mario et al. Crashworthiness assessment of a composite fuselage stanchion employing a strain rate dependent damage model. Composite Structures, v. 352, p. 1-16, 2024Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2024.118674. Acesso em: 10 nov. 2025.
APA
Miranda, M., Cini, A., Raimondo, A., & Tita, V. (2024). Crashworthiness assessment of a composite fuselage stanchion employing a strain rate dependent damage model. Composite Structures, 352, 1-16. doi:10.1016/j.compstruct.2024.118674
NLM
Miranda M, Cini A, Raimondo A, Tita V. Crashworthiness assessment of a composite fuselage stanchion employing a strain rate dependent damage model [Internet]. Composite Structures. 2024 ; 352 1-16.[citado 2025 nov. 10 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118674
Vancouver
Miranda M, Cini A, Raimondo A, Tita V. Crashworthiness assessment of a composite fuselage stanchion employing a strain rate dependent damage model [Internet]. Composite Structures. 2024 ; 352 1-16.[citado 2025 nov. 10 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118674
Artigo de periodico
Influence of the geometric parameters on the effective properties of piezoelectric composite sensors using real measurements and a new RVE (2023)
Silva, Matheus Rodrigues; Tita, Volnei ; Medeiros, Ricardo de
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, PIEZOELETRICIDADE, HOMOGENEIZAÇÃO, ENGENHARIA AERONÁUTICA
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ABNT
SILVA, Matheus Rodrigues e TITA, Volnei e MEDEIROS, Ricardo de. Influence of the geometric parameters on the effective properties of piezoelectric composite sensors using real measurements and a new RVE. Composite Structures, v. 303, p. 1-12, 2023Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2022.116292. Acesso em: 10 nov. 2025.
APA
Silva, M. R., Tita, V., & Medeiros, R. de. (2023). Influence of the geometric parameters on the effective properties of piezoelectric composite sensors using real measurements and a new RVE. Composite Structures, 303, 1-12. doi:10.1016/j.compstruct.2022.116292
NLM
Silva MR, Tita V, Medeiros R de. Influence of the geometric parameters on the effective properties of piezoelectric composite sensors using real measurements and a new RVE [Internet]. Composite Structures. 2023 ; 303 1-12.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2022.116292
Vancouver
Silva MR, Tita V, Medeiros R de. Influence of the geometric parameters on the effective properties of piezoelectric composite sensors using real measurements and a new RVE [Internet]. Composite Structures. 2023 ; 303 1-12.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2022.116292
Artigo de periodico
On the modeling of nonlinear supersonic flutter of multibay composite panels (2020)
Guimarães, Thiago A. M.; Marques, Flavio Donizeti ; Ferreira, Antonio J. M
Source: Composite Structures. Unidade: EESC
Subjects: VIBRAÇÕES DE AERONAVES, MATERIAIS COMPÓSITOS, PAINÉIS, ESTRUTURAS
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ABNT
GUIMARÃES, Thiago A. M. e MARQUES, Flavio Donizeti e FERREIRA, Antonio J. M. On the modeling of nonlinear supersonic flutter of multibay composite panels. Composite Structures, v. 232, n. Ja 2020, p. 1-6, 2020Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2019.111522. Acesso em: 10 nov. 2025.
APA
Guimarães, T. A. M., Marques, F. D., & Ferreira, A. J. M. (2020). On the modeling of nonlinear supersonic flutter of multibay composite panels. Composite Structures, 232( Ja 2020), 1-6. doi:10.1016/j.compstruct.2019.111522
NLM
Guimarães TAM, Marques FD, Ferreira AJM. On the modeling of nonlinear supersonic flutter of multibay composite panels [Internet]. Composite Structures. 2020 ; 232( Ja 2020): 1-6.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2019.111522
Vancouver
Guimarães TAM, Marques FD, Ferreira AJM. On the modeling of nonlinear supersonic flutter of multibay composite panels [Internet]. Composite Structures. 2020 ; 232( Ja 2020): 1-6.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2019.111522
Artigo de periodico
Buckling optimization of composite cylinders for axial compression: A design methodology considering a variable-axial fiber layout (2019)
Almeida Júnior, José Humberto Santos; Bittrich, Lars; Jansen, Eelco; Tita, Volnei ; Spickenheuer, Axel
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS
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ABNT
ALMEIDA JÚNIOR, José Humberto Santos et al. Buckling optimization of composite cylinders for axial compression: A design methodology considering a variable-axial fiber layout. Composite Structures, v. 222, p. 1-12, 2019Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2019.110928. Acesso em: 10 nov. 2025.
APA
Almeida Júnior, J. H. S., Bittrich, L., Jansen, E., Tita, V., & Spickenheuer, A. (2019). Buckling optimization of composite cylinders for axial compression: A design methodology considering a variable-axial fiber layout. Composite Structures, 222, 1-12. doi:10.1016/j.compstruct.2019.110928
NLM
Almeida Júnior JHS, Bittrich L, Jansen E, Tita V, Spickenheuer A. Buckling optimization of composite cylinders for axial compression: A design methodology considering a variable-axial fiber layout [Internet]. Composite Structures. 2019 ; 222 1-12.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2019.110928
Vancouver
Almeida Júnior JHS, Bittrich L, Jansen E, Tita V, Spickenheuer A. Buckling optimization of composite cylinders for axial compression: A design methodology considering a variable-axial fiber layout [Internet]. Composite Structures. 2019 ; 222 1-12.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2019.110928
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: 10 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. 10 ] 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. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2018.05.085
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
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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: 10 nov. 2025.
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 2025 nov. 10 ] 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 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2017.07.054
Artigo de periodico
Low-density polyethylene waste/recycled wood composites (2017)
Moreno, Diego David Pinzon; Saron, Clodoaldo
Source: Composite Structures. Unidade: EEL
Subjects: MATERIAIS COMPÓSITOS, FIBRAS VEGETAIS, PINHEIRO, RESÍDUOS FLORESTAIS
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ABNT
MORENO, Diego David Pinzon e SARON, Clodoaldo. Low-density polyethylene waste/recycled wood composites. Composite Structures, v. 176, p. 1152-1157, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2017.05.076. Acesso em: 10 nov. 2025.
APA
Moreno, D. D. P., & Saron, C. (2017). Low-density polyethylene waste/recycled wood composites. Composite Structures, 176, 1152-1157. doi:10.1016/j.compstruct.2017.05.076
NLM
Moreno DDP, Saron C. Low-density polyethylene waste/recycled wood composites [Internet]. Composite Structures. 2017 ;176 1152-1157.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2017.05.076
Vancouver
Moreno DDP, Saron C. Low-density polyethylene waste/recycled wood composites [Internet]. Composite Structures. 2017 ;176 1152-1157.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2017.05.076
Artigo de periodico
Evolutionary-based aeroelastic tailoring of stiffened laminate composite panels in supersonic flow regime (2017)
Marques, Flavio Donizeti ; Natarajan, S.; Ferreira, António J. M.
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, LAMINADOS, PAINÉIS, AEROELASTICIDADE DE AERONAVES
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ABNT
MARQUES, Flavio Donizeti e NATARAJAN, S. e FERREIRA, António J. M. Evolutionary-based aeroelastic tailoring of stiffened laminate composite panels in supersonic flow regime. Composite Structures, v. 167, p. 30-37, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2017.01.062. Acesso em: 10 nov. 2025.
APA
Marques, F. D., Natarajan, S., & Ferreira, A. J. M. (2017). Evolutionary-based aeroelastic tailoring of stiffened laminate composite panels in supersonic flow regime. Composite Structures, 167, 30-37. doi:10.1016/j.compstruct.2017.01.062
NLM
Marques FD, Natarajan S, Ferreira AJM. Evolutionary-based aeroelastic tailoring of stiffened laminate composite panels in supersonic flow regime [Internet]. Composite Structures. 2017 ; 167 30-37.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2017.01.062
Vancouver
Marques FD, Natarajan S, Ferreira AJM. Evolutionary-based aeroelastic tailoring of stiffened laminate composite panels in supersonic flow regime [Internet]. Composite Structures. 2017 ; 167 30-37.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2017.01.062
Artigo de periodico
A review on plate and shell theories for laminated and sandwich structures highlighting the finite element method (2016)
Caliri Junior, Mauricio Francisco; Ferreira, António Joaquim Mendes; Tita, Volnei
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, LAMINADOS, MÉTODO DOS ELEMENTOS FINITOS
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ABNT
CALIRI JUNIOR, Mauricio Francisco e FERREIRA, António Joaquim Mendes e TITA, Volnei. A review on plate and shell theories for laminated and sandwich structures highlighting the finite element method. Composite Structures, v. No 2016, p. 63-77, 2016Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2016.02.036. Acesso em: 10 nov. 2025.
APA
Caliri Junior, M. F., Ferreira, A. J. M., & Tita, V. (2016). A review on plate and shell theories for laminated and sandwich structures highlighting the finite element method. Composite Structures, No 2016, 63-77. doi:10.1016/j.compstruct.2016.02.036
NLM
Caliri Junior MF, Ferreira AJM, Tita V. A review on plate and shell theories for laminated and sandwich structures highlighting the finite element method [Internet]. Composite Structures. 2016 ; No 2016 63-77.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2016.02.036
Vancouver
Caliri Junior MF, Ferreira AJM, Tita V. A review on plate and shell theories for laminated and sandwich structures highlighting the finite element method [Internet]. Composite Structures. 2016 ; No 2016 63-77.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2016.02.036
Artigo de periodico
Different interface models for calculating the effective properties in piezoelectric composite materials with imperfect fiber-matrix adhesion (2016)
Santana, Humberto Brito; Medeiros, Ricardo de; Rodríguez Ramos, Reinaldo; Tita, Volnei
Source: Composite Structures. Unidade: EESC
Subjects: PIEZOELETRICIDADE, MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS
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ABNT
SANTANA, Humberto Brito et al. Different interface models for calculating the effective properties in piezoelectric composite materials with imperfect fiber-matrix adhesion. Composite Structures, v. 151, p. 70-80, 2016Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2016.02.003. Acesso em: 10 nov. 2025.
APA
Santana, H. B., Medeiros, R. de, Rodríguez Ramos, R., & Tita, V. (2016). Different interface models for calculating the effective properties in piezoelectric composite materials with imperfect fiber-matrix adhesion. Composite Structures, 151, 70-80. doi:10.1016/j.compstruct.2016.02.003
NLM
Santana HB, Medeiros R de, Rodríguez Ramos R, Tita V. Different interface models for calculating the effective properties in piezoelectric composite materials with imperfect fiber-matrix adhesion [Internet]. Composite Structures. 2016 ; 151 70-80.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2016.02.003
Vancouver
Santana HB, Medeiros R de, Rodríguez Ramos R, Tita V. Different interface models for calculating the effective properties in piezoelectric composite materials with imperfect fiber-matrix adhesion [Internet]. Composite Structures. 2016 ; 151 70-80.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2016.02.003
Artigo de periodico
Geometrical non-linear analysis of fiber reinforced elastic solids considering debounding (2015)
Paccola, Rodrigo Ribeiro ; Piedade Neto, Dorival; Coda, Humberto Breves
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, ESTRUTURAS, ELASTICIDADE DAS ESTRUTURAS
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ABNT
PACCOLA, Rodrigo Ribeiro e PIEDADE NETO, Dorival e CODA, Humberto Breves. Geometrical non-linear analysis of fiber reinforced elastic solids considering debounding. Composite Structures, v. 133, p. 343-357, 2015Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2015.07.097. Acesso em: 10 nov. 2025.
APA
Paccola, R. R., Piedade Neto, D., & Coda, H. B. (2015). Geometrical non-linear analysis of fiber reinforced elastic solids considering debounding. Composite Structures, 133, 343-357. doi:10.1016/j.compstruct.2015.07.097
NLM
Paccola RR, Piedade Neto D, Coda HB. Geometrical non-linear analysis of fiber reinforced elastic solids considering debounding [Internet]. Composite Structures. 2015 ; 133 343-357.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2015.07.097
Vancouver
Paccola RR, Piedade Neto D, Coda HB. Geometrical non-linear analysis of fiber reinforced elastic solids considering debounding [Internet]. Composite Structures. 2015 ; 133 343-357.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2015.07.097
Artigo de periodico
A finite element formulation for smart piezoelectric composite shells: mathematical formulation, computational analysis and experimental evaluation (2015)
Sartorato, Murilo; Medeiros, Ricardo de; Tita, Volnei
Source: Composite Structures. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, ATUADORES PIEZELÉTRICOS, MATERIAIS COMPÓSITOS
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ABNT
SARTORATO, Murilo e MEDEIROS, Ricardo de e TITA, Volnei. A finite element formulation for smart piezoelectric composite shells: mathematical formulation, computational analysis and experimental evaluation. Composite Structures, v. 127, p. 185-198, 2015Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2015.03.009. Acesso em: 10 nov. 2025.
APA
Sartorato, M., Medeiros, R. de, & Tita, V. (2015). A finite element formulation for smart piezoelectric composite shells: mathematical formulation, computational analysis and experimental evaluation. Composite Structures, 127, 185-198. doi:10.1016/j.compstruct.2015.03.009
NLM
Sartorato M, Medeiros R de, Tita V. A finite element formulation for smart piezoelectric composite shells: mathematical formulation, computational analysis and experimental evaluation [Internet]. Composite Structures. 2015 ; 127 185-198.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2015.03.009
Vancouver
Sartorato M, Medeiros R de, Tita V. A finite element formulation for smart piezoelectric composite shells: mathematical formulation, computational analysis and experimental evaluation [Internet]. Composite Structures. 2015 ; 127 185-198.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2015.03.009
Artigo de periodico
Continuous inter-laminar stresses for regular and inverse geometrically non linear dynamic and static analyses of laminated plates and shells (2015)
Coda, Humberto Breves
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, ESTRUTURAS, ELASTICIDADE DAS ESTRUTURAS
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ABNT
CODA, Humberto Breves. Continuous inter-laminar stresses for regular and inverse geometrically non linear dynamic and static analyses of laminated plates and shells. Composite Structures, v. 132, p. 406-422, 2015Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2015.05.056. Acesso em: 10 nov. 2025.
APA
Coda, H. B. (2015). Continuous inter-laminar stresses for regular and inverse geometrically non linear dynamic and static analyses of laminated plates and shells. Composite Structures, 132, 406-422. doi:10.1016/j.compstruct.2015.05.056
NLM
Coda HB. Continuous inter-laminar stresses for regular and inverse geometrically non linear dynamic and static analyses of laminated plates and shells [Internet]. Composite Structures. 2015 ; 132 406-422.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2015.05.056
Vancouver
Coda HB. Continuous inter-laminar stresses for regular and inverse geometrically non linear dynamic and static analyses of laminated plates and shells [Internet]. Composite Structures. 2015 ; 132 406-422.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2015.05.056
Artigo de periodico
Different approaches for calculating the effective elastic properties in composite materials under imperfect contact adherence (2013)
Rodríguez-Ramos, Reinaldo; Medeiros, Ricardo de; Guinovart-Díaz, Raúl; Bravo-Castillero, Julián; Otero, José Antonio; Tita, Volnei
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, HOMOGENEIZAÇÃO, MÉTODO DOS ELEMENTOS FINITOS
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ABNT
RODRÍGUEZ-RAMOS, Reinaldo et al. Different approaches for calculating the effective elastic properties in composite materials under imperfect contact adherence. Composite Structures, v. 99, p. 264-275, 2013Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2012.11.040. Acesso em: 10 nov. 2025.
APA
Rodríguez-Ramos, R., Medeiros, R. de, Guinovart-Díaz, R., Bravo-Castillero, J., Otero, J. A., & Tita, V. (2013). Different approaches for calculating the effective elastic properties in composite materials under imperfect contact adherence. Composite Structures, 99, 264-275. doi:10.1016/j.compstruct.2012.11.040
NLM
Rodríguez-Ramos R, Medeiros R de, Guinovart-Díaz R, Bravo-Castillero J, Otero JA, Tita V. Different approaches for calculating the effective elastic properties in composite materials under imperfect contact adherence [Internet]. Composite Structures. 2013 ; 99 264-275.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2012.11.040
Vancouver
Rodríguez-Ramos R, Medeiros R de, Guinovart-Díaz R, Bravo-Castillero J, Otero JA, Tita V. Different approaches for calculating the effective elastic properties in composite materials under imperfect contact adherence [Internet]. Composite Structures. 2013 ; 99 264-275.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2012.11.040
Artigo de periodico
A new damage model for composite laminates (2012)
Ribeiro, Marcelo Leite ; Tita, Volnei ; Vandepitte, Dirk
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, MATERIAIS (MODELOS), MÉTODO DOS ELEMENTOS FINITOS
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ABNT
RIBEIRO, Marcelo Leite e TITA, Volnei e VANDEPITTE, Dirk. A new damage model for composite laminates. Composite Structures, v. 94, n. Ja 2012, p. 635-642, 2012Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2011.08.031. Acesso em: 10 nov. 2025.
APA
Ribeiro, M. L., Tita, V., & Vandepitte, D. (2012). A new damage model for composite laminates. Composite Structures, 94( Ja 2012), 635-642. doi:10.1016/j.compstruct.2011.08.031
NLM
Ribeiro ML, Tita V, Vandepitte D. A new damage model for composite laminates [Internet]. Composite Structures. 2012 ; 94( Ja 2012): 635-642.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2011.08.031
Vancouver
Ribeiro ML, Tita V, Vandepitte D. A new damage model for composite laminates [Internet]. Composite Structures. 2012 ; 94( Ja 2012): 635-642.[citado 2025 nov. 10 ] Available from: https://doi.org/10.1016/j.compstruct.2011.08.031

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