Filtros : "De Marqui Júnior, Carlos" "EESC-SAA" "VIBRAÇÕES DE AERONAVES" Limpar

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  • Source: Proceedings of SPIE. Conference titles: Active and Passive Smart Structures and Integrated Systems. Unidade: EESC

    Subjects: VIBRAÇÕES DE AERONAVES, PIEZOELETRICIDADE, ENGENHARIA AERONÁUTICA

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      MOSQUERA SÁNCHEZ, Jaime Alberto e OOTANI, Nicholas K e DE MARQUI JÚNIOR, Carlos. Effects of negative capacitance circuits on the vibration attenuation performance of a nonlinear piezoelectric metamaterial. Proceedings of SPIE. Bellingham: SPIE. Disponível em: https://doi.org/10.1117/12.2612553. Acesso em: 17 jul. 2024. , 2022
    • APA

      Mosquera Sánchez, J. A., Ootani, N. K., & De Marqui Júnior, C. (2022). Effects of negative capacitance circuits on the vibration attenuation performance of a nonlinear piezoelectric metamaterial. Proceedings of SPIE. Bellingham: SPIE. doi:10.1117/12.2612553
    • NLM

      Mosquera Sánchez JA, Ootani NK, De Marqui Júnior C. Effects of negative capacitance circuits on the vibration attenuation performance of a nonlinear piezoelectric metamaterial [Internet]. Proceedings of SPIE. 2022 ; 12043 1-12.[citado 2024 jul. 17 ] Available from: https://doi.org/10.1117/12.2612553
    • Vancouver

      Mosquera Sánchez JA, Ootani NK, De Marqui Júnior C. Effects of negative capacitance circuits on the vibration attenuation performance of a nonlinear piezoelectric metamaterial [Internet]. Proceedings of SPIE. 2022 ; 12043 1-12.[citado 2024 jul. 17 ] Available from: https://doi.org/10.1117/12.2612553
  • Source: Physical Review Applied. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, PIEZOELETRICIDADE, VIBRAÇÕES DE AERONAVES, ENGENHARIA AERONÁUTICA

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      BELI, Danilo e RUZZENE, Massimo e DE MARQUI JÚNIOR, Carlos. Bridging-coupling phenomenon in linear elastic metamaterials by exploiting locally resonant metachain isomers. Physical Review Applied, v. 14, p. 1-14, 2020Tradução . . Disponível em: https://doi.org/10.1103/PhysRevApplied.14.034032. Acesso em: 17 jul. 2024.
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      Beli, D., Ruzzene, M., & De Marqui Júnior, C. (2020). Bridging-coupling phenomenon in linear elastic metamaterials by exploiting locally resonant metachain isomers. Physical Review Applied, 14, 1-14. doi:10.1103/PhysRevApplied.14.034032
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      Beli D, Ruzzene M, De Marqui Júnior C. Bridging-coupling phenomenon in linear elastic metamaterials by exploiting locally resonant metachain isomers [Internet]. Physical Review Applied. 2020 ; 14 1-14.[citado 2024 jul. 17 ] Available from: https://doi.org/10.1103/PhysRevApplied.14.034032
    • Vancouver

      Beli D, Ruzzene M, De Marqui Júnior C. Bridging-coupling phenomenon in linear elastic metamaterials by exploiting locally resonant metachain isomers [Internet]. Physical Review Applied. 2020 ; 14 1-14.[citado 2024 jul. 17 ] Available from: https://doi.org/10.1103/PhysRevApplied.14.034032
  • Conference titles: ABCM International Congress of Mechanical Engineering - COBEM. Unidade: EESC

    Subjects: VIBRAÇÕES DE AERONAVES, ENGENHARIA AERONÁUTICA

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      DOURADO, Massao Kodama et al. Active control of band gaps on a smart phononic beam. 2019, Anais.. Rio de Janeiro, RJ: ABCM, 2019. Disponível em: https://repositorio.usp.br/directbitstream/65c1d900-ef07-4607-ac17-bd9f440aa9a3/trabalho%2001%20-%20ACTIVE%20CONTROL%20OF%20BAND%20GAPS%20ON%20A%20SMART%20BEAM%20%28cobem%202019%29_removed.pdf. Acesso em: 17 jul. 2024.
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      Dourado, M. K., Gonçalves, P. J. P., De Marqui Júnior, C., & Beli, D. (2019). Active control of band gaps on a smart phononic beam. In . Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/65c1d900-ef07-4607-ac17-bd9f440aa9a3/trabalho%2001%20-%20ACTIVE%20CONTROL%20OF%20BAND%20GAPS%20ON%20A%20SMART%20BEAM%20%28cobem%202019%29_removed.pdf
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      Dourado MK, Gonçalves PJP, De Marqui Júnior C, Beli D. Active control of band gaps on a smart phononic beam [Internet]. 2019 ;[citado 2024 jul. 17 ] Available from: https://repositorio.usp.br/directbitstream/65c1d900-ef07-4607-ac17-bd9f440aa9a3/trabalho%2001%20-%20ACTIVE%20CONTROL%20OF%20BAND%20GAPS%20ON%20A%20SMART%20BEAM%20%28cobem%202019%29_removed.pdf
    • Vancouver

      Dourado MK, Gonçalves PJP, De Marqui Júnior C, Beli D. Active control of band gaps on a smart phononic beam [Internet]. 2019 ;[citado 2024 jul. 17 ] Available from: https://repositorio.usp.br/directbitstream/65c1d900-ef07-4607-ac17-bd9f440aa9a3/trabalho%2001%20-%20ACTIVE%20CONTROL%20OF%20BAND%20GAPS%20ON%20A%20SMART%20BEAM%20%28cobem%202019%29_removed.pdf
  • Source: Journal of Intelligent Material Systems and Structures. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, VIBRAÇÕES DE AERONAVES, ENGENHARIA AERONÁUTICA

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      SOUSA, Vagner Candido de e DE MARQUI JÚNIOR, Carlos. Experimental study on the aeroelastic behavior of a typical airfoil section with superelastic shape memory alloy springs. Journal of Intelligent Material Systems and Structures, v. 29, n. 4, p. 623-635, 2018Tradução . . Disponível em: https://doi.org/10.1177/1045389X17721024. Acesso em: 17 jul. 2024.
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      Sousa, V. C. de, & De Marqui Júnior, C. (2018). Experimental study on the aeroelastic behavior of a typical airfoil section with superelastic shape memory alloy springs. Journal of Intelligent Material Systems and Structures, 29( 4), 623-635. doi:10.1177/1045389X17721024
    • NLM

      Sousa VC de, De Marqui Júnior C. Experimental study on the aeroelastic behavior of a typical airfoil section with superelastic shape memory alloy springs [Internet]. Journal of Intelligent Material Systems and Structures. 2018 ; 29( 4): 623-635.[citado 2024 jul. 17 ] Available from: https://doi.org/10.1177/1045389X17721024
    • Vancouver

      Sousa VC de, De Marqui Júnior C. Experimental study on the aeroelastic behavior of a typical airfoil section with superelastic shape memory alloy springs [Internet]. Journal of Intelligent Material Systems and Structures. 2018 ; 29( 4): 623-635.[citado 2024 jul. 17 ] Available from: https://doi.org/10.1177/1045389X17721024
  • Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC

    Subjects: PIEZOELETRICIDADE, AEROELASTICIDADE DE AERONAVES, VIBRAÇÕES DE AERONAVES, ENGENHARIA MECÂNICA

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      OTSUBO, Gabriela Mayumi de Freitas e DE MARQUI JÚNIOR, Carlos. Efeito de absorvedores peizoelétricos de vibração não-lineares sobre o comportamento aeroelástico de uma seção típica. 2018, Anais.. São Carlos, SP: EESC-USP, 2018. Disponível em: http://soac.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1359/820. Acesso em: 17 jul. 2024.
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      Otsubo, G. M. de F., & De Marqui Júnior, C. (2018). Efeito de absorvedores peizoelétricos de vibração não-lineares sobre o comportamento aeroelástico de uma seção típica. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1359/820
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      Otsubo GM de F, De Marqui Júnior C. Efeito de absorvedores peizoelétricos de vibração não-lineares sobre o comportamento aeroelástico de uma seção típica [Internet]. Anais. 2018 ;[citado 2024 jul. 17 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1359/820
    • Vancouver

      Otsubo GM de F, De Marqui Júnior C. Efeito de absorvedores peizoelétricos de vibração não-lineares sobre o comportamento aeroelástico de uma seção típica [Internet]. Anais. 2018 ;[citado 2024 jul. 17 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1359/820
  • Source: Journal of Vibration and Control. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, VIBRAÇÕES DE AERONAVES, MOLAS HELICOIDAIS, ENGENHARIA AERONÁUTICA

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      SOUSA, Vagner Candido de e DE MARQUI JÚNIOR, Carlos e ELAHINIA, Mohammad H. Effect of constitutive model parameters on the aeroelastic behavior of an airfoil with shape memory alloy springs. Journal of Vibration and Control, v. 24, n. 6, p. 1065-1085, 2018Tradução . . Disponível em: https://doi.org/10.1177/1077546316657501. Acesso em: 17 jul. 2024.
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      Sousa, V. C. de, De Marqui Júnior, C., & Elahinia, M. H. (2018). Effect of constitutive model parameters on the aeroelastic behavior of an airfoil with shape memory alloy springs. Journal of Vibration and Control, 24( 6), 1065-1085. doi:10.1177/1077546316657501
    • NLM

      Sousa VC de, De Marqui Júnior C, Elahinia MH. Effect of constitutive model parameters on the aeroelastic behavior of an airfoil with shape memory alloy springs [Internet]. Journal of Vibration and Control. 2018 ; 24( 6): 1065-1085.[citado 2024 jul. 17 ] Available from: https://doi.org/10.1177/1077546316657501
    • Vancouver

      Sousa VC de, De Marqui Júnior C, Elahinia MH. Effect of constitutive model parameters on the aeroelastic behavior of an airfoil with shape memory alloy springs [Internet]. Journal of Vibration and Control. 2018 ; 24( 6): 1065-1085.[citado 2024 jul. 17 ] Available from: https://doi.org/10.1177/1077546316657501
  • Source: Journal of Intelligent Material Systems and Structures. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, VIBRAÇÕES DE AERONAVES, PIEZOELETRICIDADE, ENGENHARIA AERONÁUTICA

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      SILVA, Tarcísio Marinelli Pereira e DE MARQUI JÚNIOR, Carlos. Self-powered active control of elastic and aeroelastic oscillations using piezoelectric material. Journal of Intelligent Material Systems and Structures, v. 28, n. Ja 2017, p. 2023-2035, 2017Tradução . . Disponível em: https://doi.org/10.1177/1045389X16685448. Acesso em: 17 jul. 2024.
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      Silva, T. M. P., & De Marqui Júnior, C. (2017). Self-powered active control of elastic and aeroelastic oscillations using piezoelectric material. Journal of Intelligent Material Systems and Structures, 28( Ja 2017), 2023-2035. doi:10.1177/1045389X16685448
    • NLM

      Silva TMP, De Marqui Júnior C. Self-powered active control of elastic and aeroelastic oscillations using piezoelectric material [Internet]. Journal of Intelligent Material Systems and Structures. 2017 ; 28( Ja 2017): 2023-2035.[citado 2024 jul. 17 ] Available from: https://doi.org/10.1177/1045389X16685448
    • Vancouver

      Silva TMP, De Marqui Júnior C. Self-powered active control of elastic and aeroelastic oscillations using piezoelectric material [Internet]. Journal of Intelligent Material Systems and Structures. 2017 ; 28( Ja 2017): 2023-2035.[citado 2024 jul. 17 ] Available from: https://doi.org/10.1177/1045389X16685448
  • Source: Journal of Intelligent Material Systems and Structures. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, VIBRAÇÕES DE AERONAVES, ENGENHARIA AERONÁUTICA

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      SOUSA, Vagner Candido de e DE MARQUI JÚNIOR, Carlos. Effect of pseudoelastic hysteresis of shape memory alloy springs on the aeroelastic behavior of a typical airfoil section. Journal of Intelligent Material Systems and Structures, v. 27, n. 1, p. 117-133, 2016Tradução . . Disponível em: https://doi.org/10.1177/1045389X14563862. Acesso em: 17 jul. 2024.
    • APA

      Sousa, V. C. de, & De Marqui Júnior, C. (2016). Effect of pseudoelastic hysteresis of shape memory alloy springs on the aeroelastic behavior of a typical airfoil section. Journal of Intelligent Material Systems and Structures, 27( 1), 117-133. doi:10.1177/1045389X14563862
    • NLM

      Sousa VC de, De Marqui Júnior C. Effect of pseudoelastic hysteresis of shape memory alloy springs on the aeroelastic behavior of a typical airfoil section [Internet]. Journal of Intelligent Material Systems and Structures. 2016 ; 27( 1): 117-133.[citado 2024 jul. 17 ] Available from: https://doi.org/10.1177/1045389X14563862
    • Vancouver

      Sousa VC de, De Marqui Júnior C. Effect of pseudoelastic hysteresis of shape memory alloy springs on the aeroelastic behavior of a typical airfoil section [Internet]. Journal of Intelligent Material Systems and Structures. 2016 ; 27( 1): 117-133.[citado 2024 jul. 17 ] Available from: https://doi.org/10.1177/1045389X14563862
  • Source: AIAA Journal. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, VIBRAÇÕES DE AERONAVES, ENGENHARIA AERONÁUTICA

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      DIAS, José Augusto de Carvalho e DE MARQUI JÚNIOR, Carlos e ERTURK, Alper. Three-degree-of-freedom hybrid piezoelectric-inductive aeroelastic energy harvester exploiting a control surface. AIAA Journal, v. 53, n. 2, p. 394-404, 2015Tradução . . Disponível em: https://doi.org/10.2514/1.J053108. Acesso em: 17 jul. 2024.
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      Dias, J. A. de C., De Marqui Júnior, C., & Erturk, A. (2015). Three-degree-of-freedom hybrid piezoelectric-inductive aeroelastic energy harvester exploiting a control surface. AIAA Journal, 53( 2), 394-404. doi:10.2514/1.J053108
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      Dias JA de C, De Marqui Júnior C, Erturk A. Three-degree-of-freedom hybrid piezoelectric-inductive aeroelastic energy harvester exploiting a control surface [Internet]. AIAA Journal. 2015 ; 53( 2): 394-404.[citado 2024 jul. 17 ] Available from: https://doi.org/10.2514/1.J053108
    • Vancouver

      Dias JA de C, De Marqui Júnior C, Erturk A. Three-degree-of-freedom hybrid piezoelectric-inductive aeroelastic energy harvester exploiting a control surface [Internet]. AIAA Journal. 2015 ; 53( 2): 394-404.[citado 2024 jul. 17 ] Available from: https://doi.org/10.2514/1.J053108
  • Source: Journal of Intelligent Material Systems and Structures. Unidade: EESC

    Subjects: PIEZOELETRICIDADE, VIBRAÇÕES DE AERONAVES, AEROELASTICIDADE DE AERONAVES

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      D'ASSUNÇÃO, Douglas e DE MARQUI JÚNIOR, Carlos. Applied self-powered semi-passive control for a 2-degree-of-freedom aeroelastic typical section using shunted piezoelectric materials. Journal of Intelligent Material Systems and Structures, v. 26, n. 4, p. 373-385, 2015Tradução . . Disponível em: https://doi.org/10.1177/1045389X14526797. Acesso em: 17 jul. 2024.
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      D'Assunção, D., & De Marqui Júnior, C. (2015). Applied self-powered semi-passive control for a 2-degree-of-freedom aeroelastic typical section using shunted piezoelectric materials. Journal of Intelligent Material Systems and Structures, 26( 4), 373-385. doi:10.1177/1045389X14526797
    • NLM

      D'Assunção D, De Marqui Júnior C. Applied self-powered semi-passive control for a 2-degree-of-freedom aeroelastic typical section using shunted piezoelectric materials [Internet]. Journal of Intelligent Material Systems and Structures. 2015 ; 26( 4): 373-385.[citado 2024 jul. 17 ] Available from: https://doi.org/10.1177/1045389X14526797
    • Vancouver

      D'Assunção D, De Marqui Júnior C. Applied self-powered semi-passive control for a 2-degree-of-freedom aeroelastic typical section using shunted piezoelectric materials [Internet]. Journal of Intelligent Material Systems and Structures. 2015 ; 26( 4): 373-385.[citado 2024 jul. 17 ] Available from: https://doi.org/10.1177/1045389X14526797
  • Source: Anais. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC

    Subjects: VIBRAÇÕES DE AERONAVES, PIEZOELETRICIDADE, ENGENHARIA AERONÁUTICA

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      D'ASSUNÇÃO, Douglas e DE MARQUI JÚNIOR, Carlos. Semi-passive control of linear aeroelastic vibrations using shunted piezoelectric materials. 2013, Anais.. Rio de Janeiro, RJ: ABCM, 2013. Disponível em: https://repositorio.usp.br/directbitstream/0b71fcb7-fe39-48f9-9289-eeca80b701d0/trabalho%2031%20-%20SEMI-PASSIVE%20CONTROL%20OF%20LINEAR%20AEROELASTIC%20VIBRATIONS%20USING%20SHUNTED%20PIEZOELECTRIC%20MATERIALS%20%28COBEM%202013%29.pdf. Acesso em: 17 jul. 2024.
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      D'Assunção, D., & De Marqui Júnior, C. (2013). Semi-passive control of linear aeroelastic vibrations using shunted piezoelectric materials. In Anais. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/0b71fcb7-fe39-48f9-9289-eeca80b701d0/trabalho%2031%20-%20SEMI-PASSIVE%20CONTROL%20OF%20LINEAR%20AEROELASTIC%20VIBRATIONS%20USING%20SHUNTED%20PIEZOELECTRIC%20MATERIALS%20%28COBEM%202013%29.pdf
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      D'Assunção D, De Marqui Júnior C. Semi-passive control of linear aeroelastic vibrations using shunted piezoelectric materials [Internet]. Anais. 2013 ;[citado 2024 jul. 17 ] Available from: https://repositorio.usp.br/directbitstream/0b71fcb7-fe39-48f9-9289-eeca80b701d0/trabalho%2031%20-%20SEMI-PASSIVE%20CONTROL%20OF%20LINEAR%20AEROELASTIC%20VIBRATIONS%20USING%20SHUNTED%20PIEZOELECTRIC%20MATERIALS%20%28COBEM%202013%29.pdf
    • Vancouver

      D'Assunção D, De Marqui Júnior C. Semi-passive control of linear aeroelastic vibrations using shunted piezoelectric materials [Internet]. Anais. 2013 ;[citado 2024 jul. 17 ] Available from: https://repositorio.usp.br/directbitstream/0b71fcb7-fe39-48f9-9289-eeca80b701d0/trabalho%2031%20-%20SEMI-PASSIVE%20CONTROL%20OF%20LINEAR%20AEROELASTIC%20VIBRATIONS%20USING%20SHUNTED%20PIEZOELECTRIC%20MATERIALS%20%28COBEM%202013%29.pdf
  • Source: Anais. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC

    Subjects: PIEZOELETRICIDADE, VIBRAÇÕES DE AERONAVES, ENGENHARIA AERONÁUTICA

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      CLEMENTINO, Marcel Araujo e DE MARQUI JÚNIOR, Carlos e SILVA, Samuel da. Modeling of a commercial piezoelectric energy harvesting device through experimental identidication. 2013, Anais.. Rio de Janeiro, RJ: ABCM, 2013. Disponível em: https://repositorio.usp.br/directbitstream/efade3b9-7207-4c59-a01f-a62c7bd435f9/trabalho%2030%20-%20MODELING%20OF%20A%20COMMERCIAL%20PIEZOELECTRIC%20ENERGY%20HARVESTING%20DEVICE%20THROUGH%20EXPERIMENTAL%20IDENTIFICATION%20%28COBEM%202013%29.pdf. Acesso em: 17 jul. 2024.
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      Clementino, M. A., De Marqui Júnior, C., & Silva, S. da. (2013). Modeling of a commercial piezoelectric energy harvesting device through experimental identidication. In Anais. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/efade3b9-7207-4c59-a01f-a62c7bd435f9/trabalho%2030%20-%20MODELING%20OF%20A%20COMMERCIAL%20PIEZOELECTRIC%20ENERGY%20HARVESTING%20DEVICE%20THROUGH%20EXPERIMENTAL%20IDENTIFICATION%20%28COBEM%202013%29.pdf
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      Clementino MA, De Marqui Júnior C, Silva S da. Modeling of a commercial piezoelectric energy harvesting device through experimental identidication [Internet]. Anais. 2013 ;[citado 2024 jul. 17 ] Available from: https://repositorio.usp.br/directbitstream/efade3b9-7207-4c59-a01f-a62c7bd435f9/trabalho%2030%20-%20MODELING%20OF%20A%20COMMERCIAL%20PIEZOELECTRIC%20ENERGY%20HARVESTING%20DEVICE%20THROUGH%20EXPERIMENTAL%20IDENTIFICATION%20%28COBEM%202013%29.pdf
    • Vancouver

      Clementino MA, De Marqui Júnior C, Silva S da. Modeling of a commercial piezoelectric energy harvesting device through experimental identidication [Internet]. Anais. 2013 ;[citado 2024 jul. 17 ] Available from: https://repositorio.usp.br/directbitstream/efade3b9-7207-4c59-a01f-a62c7bd435f9/trabalho%2030%20-%20MODELING%20OF%20A%20COMMERCIAL%20PIEZOELECTRIC%20ENERGY%20HARVESTING%20DEVICE%20THROUGH%20EXPERIMENTAL%20IDENTIFICATION%20%28COBEM%202013%29.pdf
  • Source: Anais. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC

    Subjects: ENGENHARIA AERONÁUTICA, VIBRAÇÕES DE AERONAVES, AEROELASTICIDADE DE AERONAVES, TURBULÊNCIA ATMOSFÉRICA

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      SILVA, Tarcísio Marinelli Pereira e DE MARQUI JÚNIOR, Carlos. Multi-modal piezoelectric circuits for vibration suppression of a plate-like wing under atmospheric turbulence. 2013, Anais.. Rio de Janeiro, RJ: ABCM, 2013. Disponível em: https://repositorio.usp.br/directbitstream/bd99516b-3e51-4f30-b1d2-9c92aaded141/trabalho%2032%20-%20MULTI-MODAL%20PIEZOELECTRIC%20CIRCUITS%20FOR%20VIBRATION%20SUPPRESSION%20OF%20A%20PLATE-LIKE%20WING%20UNDER%20ATMOSPHERIC%20TURBULENCE%20%28COBEM%202013%29.pdf. Acesso em: 17 jul. 2024.
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      Silva, T. M. P., & De Marqui Júnior, C. (2013). Multi-modal piezoelectric circuits for vibration suppression of a plate-like wing under atmospheric turbulence. In Anais. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/bd99516b-3e51-4f30-b1d2-9c92aaded141/trabalho%2032%20-%20MULTI-MODAL%20PIEZOELECTRIC%20CIRCUITS%20FOR%20VIBRATION%20SUPPRESSION%20OF%20A%20PLATE-LIKE%20WING%20UNDER%20ATMOSPHERIC%20TURBULENCE%20%28COBEM%202013%29.pdf
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      Silva TMP, De Marqui Júnior C. Multi-modal piezoelectric circuits for vibration suppression of a plate-like wing under atmospheric turbulence [Internet]. Anais. 2013 ;[citado 2024 jul. 17 ] Available from: https://repositorio.usp.br/directbitstream/bd99516b-3e51-4f30-b1d2-9c92aaded141/trabalho%2032%20-%20MULTI-MODAL%20PIEZOELECTRIC%20CIRCUITS%20FOR%20VIBRATION%20SUPPRESSION%20OF%20A%20PLATE-LIKE%20WING%20UNDER%20ATMOSPHERIC%20TURBULENCE%20%28COBEM%202013%29.pdf
    • Vancouver

      Silva TMP, De Marqui Júnior C. Multi-modal piezoelectric circuits for vibration suppression of a plate-like wing under atmospheric turbulence [Internet]. Anais. 2013 ;[citado 2024 jul. 17 ] Available from: https://repositorio.usp.br/directbitstream/bd99516b-3e51-4f30-b1d2-9c92aaded141/trabalho%2032%20-%20MULTI-MODAL%20PIEZOELECTRIC%20CIRCUITS%20FOR%20VIBRATION%20SUPPRESSION%20OF%20A%20PLATE-LIKE%20WING%20UNDER%20ATMOSPHERIC%20TURBULENCE%20%28COBEM%202013%29.pdf
  • Source: Proceedings of SPIE. Conference titles: SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, PIEZOELETRICIDADE, VIBRAÇÕES DE AERONAVES, ENGENHARIA AERONÁUTICA

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    • ABNT

      SILVA, Tarcísio Marinelli Pereira e DE MARQUI JÚNIOR, Carlos. Passive and hybrid piezoelectric circuits to reduce induced-atmospheric turbulence vibration of a plate-like wing. Proceedings of SPIE. Bellingham, WA, USA: International Society for Optical Engineering - SPIE. Disponível em: https://doi.org/10.1117/12.2009822. Acesso em: 17 jul. 2024. , 2013
    • APA

      Silva, T. M. P., & De Marqui Júnior, C. (2013). Passive and hybrid piezoelectric circuits to reduce induced-atmospheric turbulence vibration of a plate-like wing. Proceedings of SPIE. Bellingham, WA, USA: International Society for Optical Engineering - SPIE. doi:10.1117/12.2009822
    • NLM

      Silva TMP, De Marqui Júnior C. Passive and hybrid piezoelectric circuits to reduce induced-atmospheric turbulence vibration of a plate-like wing [Internet]. Proceedings of SPIE. 2013 ; 8688 868821-1-868821-17.[citado 2024 jul. 17 ] Available from: https://doi.org/10.1117/12.2009822
    • Vancouver

      Silva TMP, De Marqui Júnior C. Passive and hybrid piezoelectric circuits to reduce induced-atmospheric turbulence vibration of a plate-like wing [Internet]. Proceedings of SPIE. 2013 ; 8688 868821-1-868821-17.[citado 2024 jul. 17 ] Available from: https://doi.org/10.1117/12.2009822

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