Mostrando 3 resultados de: 3
Design point analysis of a hybrid fuel cell gas turbine cycle for advanced distributed propulsion systems
Conference ObjectAbstract: The performance benefits of boundary layer ingestion in the case of air vehicles powered by distribuPalabras claves:Autores:Esteban Valencia, Laskaridis P., Liu C., Nalianda D., Víctor Hugo Hidalgo DíazFuentes:googlescopusDiscretized Miller approach to assess effects on boundary layer ingestion induced distortion
ArticleAbstract: The performance of propulsion configurations with boundary layer ingestion (BLI) is affected to a laPalabras claves:BLI, Correlations, Distortion, Embedded propulsors, empirical, Mean-line analysis, TurbomachineryAutores:Esteban Valencia, Laskaridis P., Nalianda D., Singh R., Víctor Hugo Hidalgo DíazFuentes:googlescopusMethodology to assess the performance of an aircraft concept with distributed propulsion and boundary layer ingestion using a parametric approach
ArticleAbstract: The performance benefits of boundary layer ingestion in aircraft with distributed propulsion have bePalabras claves:architectures, Boundary Layer Ingestion, Distributed Propulsion, Methodology, Parametric analysis, performanceAutores:Esteban Valencia, Laskaridis P., Nalianda D., Singh R.Fuentes:googlescopus