1. Repositório Institucional da Universidade Tecnológica Federal do Paraná (RIUT)
  2. GRAD - Cursos de Graduação
  3. TCC - Trabalhos de Conclusão de Curso de Graduação
  4. Guarapuava
  5. GP - Engenharia Mecânica
Use este identificador para citar ou linkar para este item: http://repositorio.utfpr.edu.br/jspui/handle/1/39129
Registro completo de metadados
Campo DCValorIdioma
dc.creatorSouza, Gabriel Suchodolak de-
dc.creatorSilva, Raquel da Cunha Ribeiro da-
dc.date.accessioned2025-12-17T19:38:57Z-
dc.date.available2025-12-17T19:38:57Z-
dc.date.issued2024-11-10-
dc.identifier.citationSOUZA, Gabriel Suchodolak de; SILVA, Raquel da Cunha Ribeiro da. In: BRAZILIAN CONGRESS OF THERMAL SCIENCES AND ENGINEERING, 20., 2024, Foz do Iguaçu. Anais eletrônicos [...]. Foz do Iguaçu: ABCM, 2024. Disponível em: doi://10.26678/ABCM.ENCIT2024.CIT24-0573 (/proceedings/view/CIT24/0573).pt_BR
dc.identifier.urihttp://repositorio.utfpr.edu.br/jspui/handle/1/39129-
dc.languageengpt_BR
dc.relation.ispartofBrazilian Congress of Thermal Sciences and Engineeringpt_BR
dc.relation.uridoi://10.26678/ABCM.ENCIT2024.CIT24-0573 (/proceedings/view/CIT24/0573)pt_BR
dc.rightsopenAccesspt_BR
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/deed.enpt_BR
dc.subjectAirfoilpt_BR
dc.subjectIce accumulationpt_BR
dc.subjectAerodynamic performancept_BR
dc.titleImpact of ice accumulation on the aerodynamic performance of the NACA 2412 airfoilpt_BR
dc.typeconferenceObjectpt_BR
dc.description.resumoThis study examines the aerodynamic performance of the NACA 2412 airfoil under icing conditions to assess its behavior in adverse weather scenarios. Ice accumulation on aircraft wings presents significant challenges to aviation safety and efficiency, impacting lift, drag, and overall flight performance. Utilizing the rhoPorousSimpleFoam solver within the OpenFOAM framework, this research simulates airflow and ice distribution on the airfoil, focusing on lift and drag coefficients. The study employs a C-shaped mesh configuration extending 15 chord lengths upstream and 20 chord lengths downstream to ensure precise results. The numerical simulations reveal that ice formation reduces the lift coefficient by up to 4.37% at 0° angle of attack and 3.12% at 12°, while increasing the drag coefficient by approximately 17.54% at 0° and 12.11% at 12°. These findings corroborate with existing literature, emphasizing the significant impact of ice on aerodynamic performance. Preliminary results also suggest modifications in pressure coefficients and airflow patterns, highlighting the intricate relationship between ice formation and aerodynamic behavior. The study underscores the necessity for effective anti-icing strategies and further research to improve aviation safety and efficiencypt_BR
dc.publisher.localGuarapuavapt_BR
dc.identifier.doidoi://10.26678/ABCM.ENCIT2024.CIT24-0573 (/proceedings/view/CIT24/0573)pt_BR
dc.publisher.countryBrasilpt_BR
dc.subject.cnpqCNPQ::ENGENHARIAS::ENGENHARIA MECANICApt_BR
dc.citation.issue20pt_BR
Aparece nas coleções:GP - Engenharia Mecânica

Arquivos associados a este item:
Arquivo Descrição TamanhoFormato 
aerodynamicperformancenacaairfoil.pdf1,91 MBAdobe PDFThumbnail
Visualizar/Abrir
Mostrar registro simples do item Recomendar este item Visualizar estatísticas


Este item está licenciada sob uma Licença Creative Commons Creative Commons