Estudo de análise operacional e perfomance para distintos aerofólios NACA em missões selecionadas
Carregando...
Arquivos
Data
2023-06-29
Autores
Título da Revista
ISSN da Revista
Título de Volume
Editor
Universidade Estadual Paulista (Unesp)
Resumo
O Trabalho de Conclusão de Curso teve como objetivo realizar uma análise operacional de diferentes aerofólios da família NACA para missões selecionadas, abordando temas como Engenharia de Sistemas e Conceitos de Operações (ConOps). Foi realizado um estudo dos aerofólios NACA, explicando sua geometria e divisão em dígitos, além de analisar três missões específicas: transporte de carga, patrulha e decolagem em pista curta, com foco em otimizar o desempenho e a eficiência das aeronaves considerando sustentação, arrasto e capacidade de carga. Através de simulações com o software XFRL5, foram avaliados parâmetros como coeficiente de sustentação, coeficiente de arrasto, eficiência aerodinâmica e comportamento em estol, visando fornecer uma análise aprofundada do impacto dos aerofólios na performance aerodinâmica de aeronaves em diferentes tipos de missões. As conclusões obtidas têm relevância no contexto de projeto e desenvolvimento de aeronaves, destacando a importância da escolha adequada do aerofólio para o cumprimento eficiente das missões, e demonstrando como os aerofólios podem influenciar significativamente o desempenho aerodinâmico em diferentes tipos de missão.
The Final Paper aimed to perform an operational analysis of different NACA airfoils for selected missions, addressing topics such as Systems Engineering and Concepts of Operations (ConOps). A study of NACA airfoils was conducted, explaining their geometry and digit classification, and analyzing three specific missions: cargo transport, patrol, and short takeoff on a runway. The focus was on optimizing the performance and efficiency of aircraft, considering lift, drag, and payload capacity. Through simulations using the XFRL5 software, parameters such as lift coefficient, drag coefficient, aerodynamic efficiency, and stall behavior were evaluated, aiming to provide an in-depth analysis of the impact of airfoils on the aerodynamic performance of aircraft in different mission types. The conclusions obtained are relevant in the context of aircraft design and development, emphasizing the importance of the appropriate selection of airfoils for efficient mission fulfillment, and demonstrating how airfoils can significantly influence the aerodynamic performance in different mission types.
The Final Paper aimed to perform an operational analysis of different NACA airfoils for selected missions, addressing topics such as Systems Engineering and Concepts of Operations (ConOps). A study of NACA airfoils was conducted, explaining their geometry and digit classification, and analyzing three specific missions: cargo transport, patrol, and short takeoff on a runway. The focus was on optimizing the performance and efficiency of aircraft, considering lift, drag, and payload capacity. Through simulations using the XFRL5 software, parameters such as lift coefficient, drag coefficient, aerodynamic efficiency, and stall behavior were evaluated, aiming to provide an in-depth analysis of the impact of airfoils on the aerodynamic performance of aircraft in different mission types. The conclusions obtained are relevant in the context of aircraft design and development, emphasizing the importance of the appropriate selection of airfoils for efficient mission fulfillment, and demonstrating how airfoils can significantly influence the aerodynamic performance in different mission types.
Descrição
Palavras-chave
Pesquisa operacional, Aerodinâmica, Aeronautica Estudo de casos