Projeto conceitual e análise de desempenho do sistema de admissão de ar em uma aeronave não convencional de combate

Projeto conceitual e análise de desempenho do sistema de admissão de ar em uma aeronave não convencional de combate

A concepção de aeronaves não convencionais a fim de alcançar um determinado desempenho ou melhoria operacional é sem dúvida um dos objetivos mais importantes da engenheira aeronáutica. Tais melhorias envolvem: redução de arrasto, redução da seção transversal, redução de ruído, redução da distância d...

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Bibliographic Details
Main Author:	Bravo Mosquera, Pedro David
Other Authors:	Catalano, Fernando Martini
Format:	Others
Language:	pt
Published:	Biblioteca Digitais de Teses e Dissertações da USP 2017
Subjects:	Aeronaves não convencionais Asa delta CFD Conceptual design Delta wing Dispositivos LEX Distorção Distortion Dorsal intake LEX devices MDO Non-conventional aircraft Projeto conceitual QFD Recuperação total de pressão Total pressure recovery
Online Access:	http://www.teses.usp.br/teses/disponiveis/18/18148/tde-03082017-131337/

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