Cargando…
Investigation of suddenly expanded flows at subsonic Mach numbers using an artificial neural networks approach
The purpose of this study is to explore two concepts: first, the use of artificial neural networks (ANN) to forecast the base pressure (β) and wall pressure (ω) originating from a suddenly expanded flow field at subsonic Mach numbers. Second, the implementation of Garson approach to determine the cr...
Autores principales: | Quadros, Jaimon Dennis, Nagpal, Chetna, Khan, Sher Afghan, Aabid, Abdul, Baig, Muneer |
---|---|
Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
Public Library of Science
2022
|
Materias: | |
Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9604976/ https://www.ncbi.nlm.nih.gov/pubmed/36288355 http://dx.doi.org/10.1371/journal.pone.0276074 |
Ejemplares similares
-
Inviscid and Viscous Interactions in Subsonic Corner Flows
por: Chung, Kung-Ming, et al.
Publicado: (2013) -
Development of a Flexible MEMS Sensor for Subsonic Flow
por: Murakami, Koichi, et al.
Publicado: (2022) -
High angle of attack aerodynamics: subsonic, transonic, and supersonic flows
por: Rom, Josef
Publicado: (1992) -
Aeroacoustics of low Mach number flows: fundamentals, analysis, and measurement
por: Glegg, Stewart A L, et al.
Publicado: (2017) -
Visualization of conventional and combusting subsonic jet instabilities
por: Kozlov, Victor, et al.
Publicado: (2016)