Mostrando 7 resultados de: 7
Assessment of distributed propulsion systems used with different aircraft configurations
Conference ObjectAbstract: The aim of the paper is to provide a top level assessment of the distributed propulsion concept applPalabras claves:Autores:Esteban Valencia, Kirner R., Laskaridis P., Wei T.J.Fuentes:scopusDesign 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:googlescopusNovel fan configuration for distributed propulsion systems with boundary layer ingestion on an hybrid wing body airframe
ArticleAbstract: The performance benefits of directly ingesting the boundary layer (BLI) on air vehicles with distribPalabras claves:conceptual design, Discretized Miller approach, Distortion tolerant fan, Rectilinear fan, Turboelectric distributed propulsionAutores:Darío A. Rodríguez, Esteban Valencia, Laskaridis P., Roumeliotis I., Víctor H. AlulemaFuentes:scopusMethodology for the assessment of distributed propulsion configurations with boundary layer ingestion using the discretized miller approach
ArticleAbstract: The growing global environmental awareness has motivated the search for more fuel- efficient aircrafPalabras claves:Boundary Layer Ingestion, Distributed Propulsion, Propulsion Configurations, Thrust splitAutores:Devaiah N., Esteban Valencia, Gray I., Laskaridis P., Liu C., Singh R.Fuentes: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:googlescopusPropulsion system analsysis using a parametric and the parallel compressor approach to model distortion in boundary layer ingestion systems
Conference ObjectAbstract: The performance benefits of boundary layer ingestion in the case of air vehicles powered by distribuPalabras claves:architectures, BLI, Parallel compressor, PROPULSIÓN, Thrust splitAutores:Devaiah N., Esteban Valencia, Laskaridis P., Liu C., Víctor Hugo Hidalgo DíazFuentes:scopus