Por favor, use este identificador para citar o enlazar este ítem: https://repositorio.ufu.br/handle/123456789/29042
Tipo de documento: Trabalho de Conclusão de Curso
Tipo de acceso: Acesso Aberto
Título: Multi-disciplinary design optimization for conceptual design of hybrid-electric aircraft
Autor: Cruz, Mateus Alves Araújo
Primer orientador: Guimarães, Thiago Augusto Machado
Primer coorientador: Silva, Higor Luis
Primer miembro de la banca: Morais, Tobias Souza
Resumen: This work presents a multidisciplinary design optimization (MDO) for general aviation and hybrid-electricaircraftdesignintegratingboxesofaerodynamics,structures,flightmechanicsand performance. The methodologies used in each box are presented and, to increase the reliability on new designs, these tools were made to minimize or not use at all any historical data. The aircraft designed is present in the general aviation market and the requirements are specified according to its competitors, taking credit of a distributed propulsion system. Furthermore, the objective-functions are minimize fuel consumption and maximum takeoff weight. The results in terms of geometry, aerodynamic parameters and performance were compared to the aircraft competitors to evaluate the accuracy of the MDO. At least, the MDO generated a final project in order to highlight the commitment relationships of a hybrid-electric aircraft in matters of the objectuve-functions definded to this project.
Palabras clave: Multidisciplinary design optimization
General aviation
Hybrid-electric aircraft
Distributed propulsion
Otimização de projeto multidisciplinar
Aviação geral
Aeronaves híbridas elétricas
Propulsão distribuída
Área (s) del CNPq: CNPQ::ENGENHARIAS
Idioma: eng
País: Brasil
Editora: Universidade Federal de Uberlândia
Cita: CRUZ, Mateus Alves Araújo. Multi-disciplinary design optimization for conceptual design of hybrid-electric aircraft. 2019. 85 f. Trabalho de Conclusão de Curso (Graduação em Engenharia Aeronáutica) - Universidade Federal de Uberlândia, Uberlândia, 2020.
URI: https://repositorio.ufu.br/handle/123456789/29042
Fecha de defensa: 20-dic-2019
Aparece en las colecciones:TCC - Engenharia Aeronáutica

Ficheros en este ítem:
Fichero Descripción TamañoFormato 
Multi-disciplinaryDesignOptimization.pdf2.88 MBAdobe PDFVista previa
Visualizar/Abrir


Los ítems de DSpace están protegidos por copyright, con todos los derechos reservados, a menos que se indique lo contrario.