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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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 02 ago. 2024.
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 2024 ago. 02 ] 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 2024 ago. 02 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2023.117756
Artigo de periodico
Evolutionary-based aeroelastic tailoring of stiffened laminate composite panels in supersonic flow regime (2017)
Marques, Flávio Donizeti; Natarajan, S.; Ferreira, António J. M.
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, LAMINADOS, PAINÉIS, AEROELASTICIDADE DE AERONAVES
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MARQUES, Flávio 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: 02 ago. 2024.
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 2024 ago. 02 ] 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 2024 ago. 02 ] Available from: https://doi.org/10.1016/j.compstruct.2017.01.062
Artigo de periodico
Zig-Zag effect without degrees of freedom in linear and non linear analysis of laminated plates and shells (2017)
Coda, Humberto Breves; Paccola, Rodrigo Ribeiro; Carrazedo, Rogério
Source: Composite Structures. Unidade: EESC
Subjects: ANÁLISE NÃO LINEAR DE ESTRUTURAS, LAMINADOS, PLACAS, ESTRUTURAS
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CODA, Humberto Breves e PACCOLA, Rodrigo Ribeiro e CARRAZEDO, Rogério. Zig-Zag effect without degrees of freedom in linear and non linear analysis of laminated plates and shells. Composite Structures, v. 161, p. 32-50, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2016.10.129. Acesso em: 02 ago. 2024.
APA
Coda, H. B., Paccola, R. R., & Carrazedo, R. (2017). Zig-Zag effect without degrees of freedom in linear and non linear analysis of laminated plates and shells. Composite Structures, 161, 32-50. doi:10.1016/j.compstruct.2016.10.129
NLM
Coda HB, Paccola RR, Carrazedo R. Zig-Zag effect without degrees of freedom in linear and non linear analysis of laminated plates and shells [Internet]. Composite Structures. 2017 ; 161 32-50.[citado 2024 ago. 02 ] Available from: https://doi.org/10.1016/j.compstruct.2016.10.129
Vancouver
Coda HB, Paccola RR, Carrazedo R. Zig-Zag effect without degrees of freedom in linear and non linear analysis of laminated plates and shells [Internet]. Composite Structures. 2017 ; 161 32-50.[citado 2024 ago. 02 ] Available from: https://doi.org/10.1016/j.compstruct.2016.10.129
Artigo de periodico
Triangular based prismatic finite element for the analysis of orthotropic laminated beams, plates and shells (2017)
Carrazedo, Rogério ; Coda, Humberto Breves
Source: Composite Structures. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, VIGAS, LAMINADOS, ESTRUTURAS
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CARRAZEDO, Rogério e CODA, Humberto Breves. Triangular based prismatic finite element for the analysis of orthotropic laminated beams, plates and shells. Composite Structures, v. 168, p. 234-246, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2017.02.027. Acesso em: 02 ago. 2024.
APA
Carrazedo, R., & Coda, H. B. (2017). Triangular based prismatic finite element for the analysis of orthotropic laminated beams, plates and shells. Composite Structures, 168, 234-246. doi:10.1016/j.compstruct.2017.02.027
NLM
Carrazedo R, Coda HB. Triangular based prismatic finite element for the analysis of orthotropic laminated beams, plates and shells [Internet]. Composite Structures. 2017 ; 168 234-246.[citado 2024 ago. 02 ] Available from: https://doi.org/10.1016/j.compstruct.2017.02.027
Vancouver
Carrazedo R, Coda HB. Triangular based prismatic finite element for the analysis of orthotropic laminated beams, plates and shells [Internet]. Composite Structures. 2017 ; 168 234-246.[citado 2024 ago. 02 ] Available from: https://doi.org/10.1016/j.compstruct.2017.02.027
Artigo de periodico
Through-the-thickness stress profiles in laminated composite and sandwich structure plates via unified formulation (2016)
Caliri Junior, Mauricio Francisco; Ferreira, Antonio Joaquim Mendes; Tita, Volnei
Source: Composites Part B. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, LAMINADOS, MÉTODO DOS ELEMENTOS FINITOS
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CALIRI JUNIOR, Mauricio Francisco e FERREIRA, Antonio Joaquim Mendes e TITA, Volnei. Through-the-thickness stress profiles in laminated composite and sandwich structure plates via unified formulation. Composites Part B, v. 107, p. 29-42, 2016Tradução . . Disponível em: https://doi.org/10.1016/j.compositesb.2016.09.055. Acesso em: 02 ago. 2024.
APA
Caliri Junior, M. F., Ferreira, A. J. M., & Tita, V. (2016). Through-the-thickness stress profiles in laminated composite and sandwich structure plates via unified formulation. Composites Part B, 107, 29-42. doi:10.1016/j.compositesb.2016.09.055
NLM
Caliri Junior MF, Ferreira AJM, Tita V. Through-the-thickness stress profiles in laminated composite and sandwich structure plates via unified formulation [Internet]. Composites Part B. 2016 ; 107 29-42.[citado 2024 ago. 02 ] Available from: https://doi.org/10.1016/j.compositesb.2016.09.055
Vancouver
Caliri Junior MF, Ferreira AJM, Tita V. Through-the-thickness stress profiles in laminated composite and sandwich structure plates via unified formulation [Internet]. Composites Part B. 2016 ; 107 29-42.[citado 2024 ago. 02 ] Available from: https://doi.org/10.1016/j.compositesb.2016.09.055
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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 02 ago. 2024.
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 2024 ago. 02 ] 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 2024 ago. 02 ] Available from: https://doi.org/10.1016/j.compstruct.2016.02.036

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