Zobrazeno 1 - 10
of 19
pro vyhledávání: '"Guilherme Araújo Lima da Silva"'
Autor:
Otavio de Mattos Silvares, Euryale Jorge de Godoy Jesus Zerbini, Guilherme Araújo Lima da Silva
Publikováno v:
Journal of Aircraft. 44:634-641
We present the implementation and results of an airfoil electrothermal anti-ice mathematical model. From flowfield and supercooled water droplet impingement data up to electrical power density distribution, the numerical code is able to predict airfo
Autor:
Otavio de Mattos Silvares, Guilherme Araújo Lima da Silva, Euryale Jorge Godoy de Jesus Zerbini
Publikováno v:
Journal of Aircraft. 44:627-633
A mathematical model was developed to both describe an airfoil electrothermal anti-ice system operation and enable prediction of its main parameters. A reference case was chosen to define the mathematical model and support the results validation. The
Autor:
Guilherme Araújo Lima da Silva, Euryale Jorge Godoy de Jesus Zerbini, Otavio de Mattos Silvares, Luciano Martinez Stefanini
Publikováno v:
AIAA Atmospheric and Space Environments Conference.
yz thalpy during glaze ice accretion. Most of the airfoil icing prediction codes use a heat transfer calculation procedure based on the classical integral evaluation of the boundary layer. These icing codes consider a smooth surface in laminar regime
Publikováno v:
Biblioteca Digital de Teses e Dissertações da USPUniversidade de São PauloUSP.
Há a necessidade de prevenir formação de gelo nas asas e nos estabilizadores de aeronaves, pois as formas de gelo podem causar a degradação do desempenho aerodinâmico, o aumento de peso, bem como dificuldades de controle e manobra que, em casos
Publikováno v:
Biblioteca Digital de Teses e Dissertações da USP
Universidade de São Paulo (USP)
instacron:USP
Universidade de São Paulo (USP)
instacron:USP
Há a necessidade de prevenir formação de gelo nas asas e nos estabilizadores de aeronaves, pois as formas de gelo podem causar a degradação do desempenho aerodinâmico, o aumento de peso, bem como dificuldades de controle e manobra que, em casos
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1976b45dac310cfb017ea7a4e79b9a05
Autor:
Otavio de Mattos Silvares, Euryale Jorge Godoy de Jesus Zerbini, Luciano Martinez Stefanini, Guilherme Araújo Lima da Silva
Publikováno v:
46th AIAA Aerospace Sciences Meeting and Exhibit.
Various classic icing codes have been developed and used by the aircraft manufacturers to predict the ice shapes evolution in non-protected airfoil surfaces. These codes apply boundary layer integral analysis, based on sand grain roughness, to estima
Autor:
Otavio de Mattos Silvares, Guilherme Araújo Lima da Silva, Euryale Jorge Godoy de Jesus Zerbini
Publikováno v:
46th AIAA Aerospace Sciences Meeting and Exhibit.
Under icing conditions, it is necessary to heat and control the temperature of the airfoil surface at leading edge region to prevent ice formation. The thermal anti-ice system balances mainly the evaporative cooling effects, which are caused by the c
Autor:
Euryale Jorge Godoy de Jesus Zerbini, Otavio de Mattos Silvares, Guilherme Araújo Lima da Silva
Publikováno v:
International Symposium on Advances in Computational Heat Transfer.
Autor:
Guilherme Araújo Lima da Silva, Rodgrigo Hoffmann Domingos, Luis Gustavo Trapp, William Campo, Marcelo Pustelnik, Luis Santos
Publikováno v:
SAE Technical Paper Series.
Publikováno v:
45th AIAA Aerospace Sciences Meeting and Exhibit.