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Numerical Simulation of Supersonic Gap Flow

Various gaps in the surface of the supersonic aircraft have a significant effect on airflows. In order to predict the effects of attack angle, Mach number and width-to-depth ratio of gap on the local aerodynamic heating environment of supersonic flow, two-dimensional compressible Navier-Stokes equat...

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Detalles Bibliográficos
Autores principales:	Jing, Xu, Haiming, Huang, Guo, Huang, Song, Mo
Formato:	Online Artículo Texto
Lenguaje:	English
Publicado:	Public Library of Science 2015
Materias:	Research Article
Acceso en línea:	https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4312046/ https://www.ncbi.nlm.nih.gov/pubmed/25635395 http://dx.doi.org/10.1371/journal.pone.0117012

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