Filtros : "Proceedings: Geospatial Data and Geographical Information Science" "ENGENHARIA AERONÁUTICA" Removido: "CAURIN, GLAUCO AUGUSTO DE PAULA" Limpar

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  • Source: Proceedings. Conference titles: IEEE/RSJ International Conference on Intelligent Robots and Systems - IROS. Unidade: EESC

    Subjects: TRAJETÓRIA, APRENDIZAGEM PROFUNDA, VOO (ENGENHARIA AERONÁUTICA), REDES NEURAIS, ENGENHARIA AERONÁUTICA

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      ROCHA, Lidia et al. Enhancing safety via deep reinforcement learning in trajectory planning for agile flights in unknown environments. 2024, Anais.. Piscataway, NJ, USA: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2024. Disponível em: https://dx.doi.org/10.1109/IROS58592.2024.10801910. Acesso em: 29 nov. 2025.
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      Rocha, L., Bidinotto, J. H., Heintz, F., Tiger, M., & Vivaldini, K. C. T. (2024). Enhancing safety via deep reinforcement learning in trajectory planning for agile flights in unknown environments. In Proceedings. Piscataway, NJ, USA: Escola de Engenharia de São Carlos, Universidade de São Paulo. doi:10.1109/IROS58592.2024.10801910
    • NLM

      Rocha L, Bidinotto JH, Heintz F, Tiger M, Vivaldini KCT. Enhancing safety via deep reinforcement learning in trajectory planning for agile flights in unknown environments [Internet]. Proceedings. 2024 ;[citado 2025 nov. 29 ] Available from: https://dx.doi.org/10.1109/IROS58592.2024.10801910
    • Vancouver

      Rocha L, Bidinotto JH, Heintz F, Tiger M, Vivaldini KCT. Enhancing safety via deep reinforcement learning in trajectory planning for agile flights in unknown environments [Internet]. Proceedings. 2024 ;[citado 2025 nov. 29 ] Available from: https://dx.doi.org/10.1109/IROS58592.2024.10801910
  • Source: Proceedings. Conference titles: IEEE RAS/EMBS International Conference for Biomedical Robotics and Biomechatronics - BioRob. Unidade: EESC

    Assunto: ENGENHARIA AERONÁUTICA

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      GODOY, Ricardo Vilela de et al. Electromyography-based, robust hand motion classification employing temporal multi-channel vision transformers. 2022, Anais.. Piscataway, NJ, USA: IEEE, 2022. Disponível em: https://doi.org/10.1109/BioRob52689.2022.9925307. Acesso em: 29 nov. 2025.
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      Godoy, R. V. de, Lahr, G. J. G., Dwivedi, A., Reis, ^T. ^J. ^S. ^dos, Polegato, P. H., Becker, M., et al. (2022). Electromyography-based, robust hand motion classification employing temporal multi-channel vision transformers. In Proceedings. Piscataway, NJ, USA: IEEE. doi:10.1109/BioRob52689.2022.9925307
    • NLM

      Godoy RV de, Lahr GJG, Dwivedi A, Reis ^T^J^S^dos, Polegato PH, Becker M, Caurin GA de P, Liarokapis M. Electromyography-based, robust hand motion classification employing temporal multi-channel vision transformers [Internet]. Proceedings. 2022 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.1109/BioRob52689.2022.9925307
    • Vancouver

      Godoy RV de, Lahr GJG, Dwivedi A, Reis ^T^J^S^dos, Polegato PH, Becker M, Caurin GA de P, Liarokapis M. Electromyography-based, robust hand motion classification employing temporal multi-channel vision transformers [Internet]. Proceedings. 2022 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.1109/BioRob52689.2022.9925307
  • Source: Proceedings. Conference titles: AIAA Aviation Forum. Unidade: EESC

    Subjects: VOO (ENGENHARIA AERONÁUTICA), ACIDENTES, SIMULADORES DE VOO, ENGENHARIA AERONÁUTICA

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      MACEDO, João Paulo Costa Antunes de e BIDINOTTO, Jorge Henrique e BROMFIELD, Michael A. Loss of control in flight: comparing qualitative pilot opinion with quantitative flight data. 2020, Anais.. Reston, VA, USA: AIAA, 2020. Disponível em: https://doi.org/10.2514/6.2020-2911. Acesso em: 29 nov. 2025.
    • APA

      Macedo, J. P. C. A. de, Bidinotto, J. H., & Bromfield, M. A. (2020). Loss of control in flight: comparing qualitative pilot opinion with quantitative flight data. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2020-2911
    • NLM

      Macedo JPCA de, Bidinotto JH, Bromfield MA. Loss of control in flight: comparing qualitative pilot opinion with quantitative flight data [Internet]. Proceedings. 2020 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2020-2911
    • Vancouver

      Macedo JPCA de, Bidinotto JH, Bromfield MA. Loss of control in flight: comparing qualitative pilot opinion with quantitative flight data [Internet]. Proceedings. 2020 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2020-2911
  • Source: Proceedings. Conference titles: AIAA Propulsion and Energy Forum. Unidade: EESC

    Subjects: ENGENHARIA AERONÁUTICA, AERODINÂMICA DE AERONAVES

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      BOCCATO, Bruno Ribeiro e BRAVO MOSQUERA, Pedro David e CATALANO, Fernando Martini. Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-4200. Acesso em: 29 nov. 2025.
    • APA

      Boccato, B. R., Bravo Mosquera, P. D., & Catalano, F. M. (2019). Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-4200
    • NLM

      Boccato BR, Bravo Mosquera PD, Catalano FM. Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-4200
    • Vancouver

      Boccato BR, Bravo Mosquera PD, Catalano FM. Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-4200
  • Source: Proceedings. Conference titles: International Congress and Exhibition on Noise Control Engineering. Unidade: EESC

    Subjects: FUSELAGEM DE AERONAVES, AEROACÚSTICA, ENGENHARIA AERONÁUTICA

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      BOTERO BOLÍVAR, Laura et al. Numerical analysis of the instabilities behind a blunt slat trailing-edge. 2019, Anais.. Madrid, Espanha: SEA, 2019. Disponível em: https://repositorio.usp.br/directbitstream/dcd29da1-7d14-4d78-a1ae-543b60c12178/trabalho%2003%20-%20Numerical%20analysis%20of%20the%20instabilities%20behind%20a%20blunt%20slat%20trailing-edge%20%28internoise%202019%29.pdf. Acesso em: 29 nov. 2025.
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      Botero Bolívar, L., Acevedo Giraldo, D., Pereira, L. T. L., Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2019). Numerical analysis of the instabilities behind a blunt slat trailing-edge. In Proceedings. Madrid, Espanha: SEA. Recuperado de https://repositorio.usp.br/directbitstream/dcd29da1-7d14-4d78-a1ae-543b60c12178/trabalho%2003%20-%20Numerical%20analysis%20of%20the%20instabilities%20behind%20a%20blunt%20slat%20trailing-edge%20%28internoise%202019%29.pdf
    • NLM

      Botero Bolívar L, Acevedo Giraldo D, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Numerical analysis of the instabilities behind a blunt slat trailing-edge [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/dcd29da1-7d14-4d78-a1ae-543b60c12178/trabalho%2003%20-%20Numerical%20analysis%20of%20the%20instabilities%20behind%20a%20blunt%20slat%20trailing-edge%20%28internoise%202019%29.pdf
    • Vancouver

      Botero Bolívar L, Acevedo Giraldo D, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Numerical analysis of the instabilities behind a blunt slat trailing-edge [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/dcd29da1-7d14-4d78-a1ae-543b60c12178/trabalho%2003%20-%20Numerical%20analysis%20of%20the%20instabilities%20behind%20a%20blunt%20slat%20trailing-edge%20%28internoise%202019%29.pdf
  • Source: Proceedings. Conference titles: AIAA Aviation Forum. Unidade: EESC

    Subjects: AEROACÚSTICA, SLATS, ENGENHARIA AERONÁUTICA

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      HIMENO, Fernando Henrique Tadashi et al. Recirculating coherent structures inside the cove of a bulb sealed slat. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-3695. Acesso em: 29 nov. 2025.
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      Himeno, F. H. T., Amaral, F. R. do, Souza, D. S., Rodriguez, D., & Medeiros, M. A. F. de. (2019). Recirculating coherent structures inside the cove of a bulb sealed slat. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-3695
    • NLM

      Himeno FHT, Amaral FR do, Souza DS, Rodriguez D, Medeiros MAF de. Recirculating coherent structures inside the cove of a bulb sealed slat [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-3695
    • Vancouver

      Himeno FHT, Amaral FR do, Souza DS, Rodriguez D, Medeiros MAF de. Recirculating coherent structures inside the cove of a bulb sealed slat [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-3695
  • Source: Proceedings. Conference titles: International Congress and Exhibition on Noise Control Engineering. Unidade: EESC

    Subjects: FUSELAGEM DE AERONAVES, AEROACÚSTICA, ENGENHARIA AERONÁUTICA

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      ACEVEDO GIRALDO, Daniel et al. Experimental and numerical aeroacoustic analyses of a large-scale flap side-edge model. 2019, Anais.. Madrid, Espanha: SEA, 2019. Disponível em: https://repositorio.usp.br/directbitstream/3de08e9e-beab-4d74-a11f-1565256469b2/trabalho%2004%20-%20Experimental%20and%20Numerical%20Aeroacoustic%20Analyses%20of%20a%20Large-scale%20Flap%20Side-edge%20Model%20%28internoise%202019%29_removed.pdf. Acesso em: 29 nov. 2025.
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      Acevedo Giraldo, D., Botero Bolívar, L., Pereira, L. T. L., Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2019). Experimental and numerical aeroacoustic analyses of a large-scale flap side-edge model. In Proceedings. Madrid, Espanha: SEA. Recuperado de https://repositorio.usp.br/directbitstream/3de08e9e-beab-4d74-a11f-1565256469b2/trabalho%2004%20-%20Experimental%20and%20Numerical%20Aeroacoustic%20Analyses%20of%20a%20Large-scale%20Flap%20Side-edge%20Model%20%28internoise%202019%29_removed.pdf
    • NLM

      Acevedo Giraldo D, Botero Bolívar L, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Experimental and numerical aeroacoustic analyses of a large-scale flap side-edge model [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/3de08e9e-beab-4d74-a11f-1565256469b2/trabalho%2004%20-%20Experimental%20and%20Numerical%20Aeroacoustic%20Analyses%20of%20a%20Large-scale%20Flap%20Side-edge%20Model%20%28internoise%202019%29_removed.pdf
    • Vancouver

      Acevedo Giraldo D, Botero Bolívar L, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Experimental and numerical aeroacoustic analyses of a large-scale flap side-edge model [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/3de08e9e-beab-4d74-a11f-1565256469b2/trabalho%2004%20-%20Experimental%20and%20Numerical%20Aeroacoustic%20Analyses%20of%20a%20Large-scale%20Flap%20Side-edge%20Model%20%28internoise%202019%29_removed.pdf
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC

    Subjects: ENGENHARIA AERONÁUTICA, AEROACÚSTICA, TERCEIRA DIMENSÃO

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      REIS, Danillo Cafaldo dos et al. A study on the 3D effects of slat cove fillers. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-2406. Acesso em: 29 nov. 2025.
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      Reis, D. C. dos, Coelho, E. L. C., Pereira, L. T. L., Catalano, F. M., & Lima, L. S. de M. (2019). A study on the 3D effects of slat cove fillers. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-2406
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      Reis DC dos, Coelho ELC, Pereira LTL, Catalano FM, Lima LS de M. A study on the 3D effects of slat cove fillers [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-2406
    • Vancouver

      Reis DC dos, Coelho ELC, Pereira LTL, Catalano FM, Lima LS de M. A study on the 3D effects of slat cove fillers [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-2406
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC

    Subjects: ENGENHARIA AERONÁUTICA, AEROACÚSTICA

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      PAGANI JÚNIOR, Carlos do Carmo e CALDAS, Luciano Coutinho e MEDEIROS, Marcello Augusto Faraco de. An experimental and numeric investigation towards a reliable acoustic pressure level estimate using phased-array techniques. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-2700. Acesso em: 29 nov. 2025.
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      Pagani Júnior, C. do C., Caldas, L. C., & Medeiros, M. A. F. de. (2019). An experimental and numeric investigation towards a reliable acoustic pressure level estimate using phased-array techniques. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-2700
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      Pagani Júnior C do C, Caldas LC, Medeiros MAF de. An experimental and numeric investigation towards a reliable acoustic pressure level estimate using phased-array techniques [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-2700
    • Vancouver

      Pagani Júnior C do C, Caldas LC, Medeiros MAF de. An experimental and numeric investigation towards a reliable acoustic pressure level estimate using phased-array techniques [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-2700
  • Source: Proceedings. Conference titles: AIAA Propulsion and Energy Forum. Unidade: EESC

    Subjects: ENGENHARIA AERONÁUTICA, ASAS DE AERONAVES, AERODINÂMICA DE AERONAVES

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      BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-3850. Acesso em: 29 nov. 2025.
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      Bravo Mosquera, P. D., Cerón Muñoz, H. D., & Catalano, F. M. (2019). Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-3850
    • NLM

      Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-3850
    • Vancouver

      Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-3850
  • Source: Proceedings. Conference titles: AIAA Aviation Forum. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA

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      MATHIAS, Marlon Sproesser e MEDEIROS, Marcello Augusto Faraco de. Global instability analysis of a boundary layer flow over a small cavity. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-3535. Acesso em: 29 nov. 2025.
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      Mathias, M. S., & Medeiros, M. A. F. de. (2019). Global instability analysis of a boundary layer flow over a small cavity. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-3535
    • NLM

      Mathias MS, Medeiros MAF de. Global instability analysis of a boundary layer flow over a small cavity [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-3535
    • Vancouver

      Mathias MS, Medeiros MAF de. Global instability analysis of a boundary layer flow over a small cavity [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-3535
  • Source: Proceedings. Conference titles: AIAA Propulsion and Energy Forum. Unidade: EESC

    Subjects: TRANSFERÊNCIA DE CALOR, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA

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      RIBEIRO, Daniel Garcia e BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío. Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://repositorio.usp.br/directbitstream/558bdbaf-a0df-406a-aee5-d60273db8fa1/trabalho%2001%20-%20Heat%20transfer%20effects%20on%20aerodynamic%20performance%20of%20a%20S809%20airfoil%20for%20wind%20turbine%20application%20%28AIAA%20Propulsion%20and%20Energy%202019%20Forum%29.pdf. Acesso em: 29 nov. 2025.
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      Ribeiro, D. G., Bravo Mosquera, P. D., & Cerón Muñoz, H. D. (2019). Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/558bdbaf-a0df-406a-aee5-d60273db8fa1/trabalho%2001%20-%20Heat%20transfer%20effects%20on%20aerodynamic%20performance%20of%20a%20S809%20airfoil%20for%20wind%20turbine%20application%20%28AIAA%20Propulsion%20and%20Energy%202019%20Forum%29.pdf
    • NLM

      Ribeiro DG, Bravo Mosquera PD, Cerón Muñoz HD. Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/558bdbaf-a0df-406a-aee5-d60273db8fa1/trabalho%2001%20-%20Heat%20transfer%20effects%20on%20aerodynamic%20performance%20of%20a%20S809%20airfoil%20for%20wind%20turbine%20application%20%28AIAA%20Propulsion%20and%20Energy%202019%20Forum%29.pdf
    • Vancouver

      Ribeiro DG, Bravo Mosquera PD, Cerón Muñoz HD. Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/558bdbaf-a0df-406a-aee5-d60273db8fa1/trabalho%2001%20-%20Heat%20transfer%20effects%20on%20aerodynamic%20performance%20of%20a%20S809%20airfoil%20for%20wind%20turbine%20application%20%28AIAA%20Propulsion%20and%20Energy%202019%20Forum%29.pdf
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC

    Subjects: AEROACÚSTICA, ENGENHARIA AERONÁUTICA

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      SPILLERE, André M. N. et al. Inlet liner design for a fan noise test rig. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-2724. Acesso em: 29 nov. 2025.
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      Spillere, A. M. N., Braga, D. S., Seki, L. A., Bonomo, L. A., Cordioli, J. A., Rocamora Junior, B. M., et al. (2019). Inlet liner design for a fan noise test rig. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-2724
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      Spillere AMN, Braga DS, Seki LA, Bonomo LA, Cordioli JA, Rocamora Junior BM, Greco Júnior PC, Reis DC dos, Coelho ELC. Inlet liner design for a fan noise test rig [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-2724
    • Vancouver

      Spillere AMN, Braga DS, Seki LA, Bonomo LA, Cordioli JA, Rocamora Junior BM, Greco Júnior PC, Reis DC dos, Coelho ELC. Inlet liner design for a fan noise test rig [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2019-2724
  • 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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      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: 29 nov. 2025.
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      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
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      Ferreira GFO, Ribeiro ML, Ferreira AJM, Tita V. Computational analysis for carbon-epoxy plates damaged by low-velocity impact [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] 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 2025 nov. 29 ] 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
  • Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC

    Subjects: AEROACÚSTICA, KRIGAGEM, ENGENHARIA AERONÁUTICA

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      GIGENA CUENCA, Rafael e GRECO JÚNIOR, Paulo Celso e MARTÍNEZ ROCAMORA JUNIOR, Bernardo. Parametric investigation of EESC-USP aeroacoustic fan rig. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/dac92081-b591-461c-b6c2-36d72d42eab6/AP8F33~1.PDF. Acesso em: 29 nov. 2025.
    • APA

      Gigena Cuenca, R., Greco Júnior, P. C., & Martínez Rocamora Junior, B. (2018). Parametric investigation of EESC-USP aeroacoustic fan rig. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/dac92081-b591-461c-b6c2-36d72d42eab6/AP8F33~1.PDF
    • NLM

      Gigena Cuenca R, Greco Júnior PC, Martínez Rocamora Junior B. Parametric investigation of EESC-USP aeroacoustic fan rig [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/dac92081-b591-461c-b6c2-36d72d42eab6/AP8F33~1.PDF
    • Vancouver

      Gigena Cuenca R, Greco Júnior PC, Martínez Rocamora Junior B. Parametric investigation of EESC-USP aeroacoustic fan rig [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/dac92081-b591-461c-b6c2-36d72d42eab6/AP8F33~1.PDF
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC

    Subjects: AEROACÚSTICA, SLATS, ENGENHARIA AERONÁUTICA

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      BOTERO BOLÍVAR, Laura et al. Parametric analysis of the influence of slat geometry on acoustic noise. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3593. Acesso em: 29 nov. 2025.
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      Botero Bolívar, L., Pereira, L. T. L., Acevedo Giraldo, D., Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2018). Parametric analysis of the influence of slat geometry on acoustic noise. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3593
    • NLM

      Botero Bolívar L, Pereira LTL, Acevedo Giraldo D, Catalano FM, Reis DC dos, Coelho ELC. Parametric analysis of the influence of slat geometry on acoustic noise [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-3593
    • Vancouver

      Botero Bolívar L, Pereira LTL, Acevedo Giraldo D, Catalano FM, Reis DC dos, Coelho ELC. Parametric analysis of the influence of slat geometry on acoustic noise [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-3593
  • Source: Proceedings. Conference titles: AAIA Aerospace Sciences Meeting. Unidade: EESC

    Subjects: TRENS DE POUSO, ENGENHARIA AERONÁUTICA, AERODINÂMICA DE AERONAVES, AEROACÚSTICA

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      REGO, Leandro Falcão Loureiro et al. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-0759. Acesso em: 29 nov. 2025.
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      Rego, L. F. L., Pereira, L. T. L., Catalano, F. M., Speth, R., Bent, P., & Fregnani, J. A. (2018). Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-0759
    • NLM

      Rego LFL, Pereira LTL, Catalano FM, Speth R, Bent P, Fregnani JA. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-0759
    • Vancouver

      Rego LFL, Pereira LTL, Catalano FM, Speth R, Bent P, Fregnani JA. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-0759
  • Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC

    Subjects: DINÂMICA DE VOO, ENGENHARIA AERONÁUTICA

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      DAUD FILHO, Antonio Carlos e BELO, Eduardo Morgado. Flight dynamics modeling and trim curves of a conceptual semi-tandem wing VTOL UAV. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/987dd969-af4d-49be-a001-64ec8719b596/trabalho%2001%20-%20FLIGHT%20DYNAMICS%20MODELING%20AND%20TRIM%20CURVES%20OF%20A%20CONCEPTUAL%20SEMI-TANDEM%20WING%20VTOL%20UAV%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf. Acesso em: 29 nov. 2025.
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      Daud Filho, A. C., & Belo, E. M. (2018). Flight dynamics modeling and trim curves of a conceptual semi-tandem wing VTOL UAV. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/987dd969-af4d-49be-a001-64ec8719b596/trabalho%2001%20-%20FLIGHT%20DYNAMICS%20MODELING%20AND%20TRIM%20CURVES%20OF%20A%20CONCEPTUAL%20SEMI-TANDEM%20WING%20VTOL%20UAV%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf
    • NLM

      Daud Filho AC, Belo EM. Flight dynamics modeling and trim curves of a conceptual semi-tandem wing VTOL UAV [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/987dd969-af4d-49be-a001-64ec8719b596/trabalho%2001%20-%20FLIGHT%20DYNAMICS%20MODELING%20AND%20TRIM%20CURVES%20OF%20A%20CONCEPTUAL%20SEMI-TANDEM%20WING%20VTOL%20UAV%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf
    • Vancouver

      Daud Filho AC, Belo EM. Flight dynamics modeling and trim curves of a conceptual semi-tandem wing VTOL UAV [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/987dd969-af4d-49be-a001-64ec8719b596/trabalho%2001%20-%20FLIGHT%20DYNAMICS%20MODELING%20AND%20TRIM%20CURVES%20OF%20A%20CONCEPTUAL%20SEMI-TANDEM%20WING%20VTOL%20UAV%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC

    Subjects: FLAPS, AEROACÚSTICA, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA

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      ACEVEDO GIRALDO, Daniel et al. Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3799. Acesso em: 29 nov. 2025.
    • APA

      Acevedo Giraldo, D., Botero Bolívar, L., Pereira, L. T. L., Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2018). Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3799
    • NLM

      Acevedo Giraldo D, Botero Bolívar L, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-3799
    • Vancouver

      Acevedo Giraldo D, Botero Bolívar L, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.2514/6.2018-3799
  • Source: Proceedings. Conference titles: Congreso Latinoamericano de Ingeniería Mecánica - COLIM. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, TURBINAS, ENERGIA EÓLICA, ENGENHARIA AERONÁUTICA

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      PARRA PEÑUELA, Héctor e GÓMEZ RIVERA, William e CERÓN MUÑOZ, Hernán Darío. Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica. 2018, Anais.. Pamplona, Colômbia: Universidad Pamplona, 2018. Disponível em: https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf. Acesso em: 29 nov. 2025.
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      Parra Peñuela, H., Gómez Rivera, W., & Cerón Muñoz, H. D. (2018). Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica. In Proceedings. Pamplona, Colômbia: Universidad Pamplona. Recuperado de https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf
    • NLM

      Parra Peñuela H, Gómez Rivera W, Cerón Muñoz HD. Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf
    • Vancouver

      Parra Peñuela H, Gómez Rivera W, Cerón Muñoz HD. Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf

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