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AIAA Propulsion and Energy 2020 Forum(3)
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scopus(9)
A CAD-free methodology for volume and mass properties computation of 3-D lifting surfaces and wing-box structures
ArticleAbstract: The geometry, volume, and mass properties (GVM) of lifting surfaces and wing box structures play anPalabras claves:3-d modeling, Aircraft design, CAD-free, Geometry discretization, Lifting surface CAD/CAE, Volume and mass computationAutores:Darío A. Rodríguez, Esteban Valencia, Víctor H. Alulema, Víctor Hugo Hidalgo DíazFuentes:scopusAerodynamic design and testing of a ram air turbine for small fixed-wing uavs
Conference ObjectAbstract: Ram Air Turbines (RAT) have been widely studied as auxiliary power units for civil aircraft. HoweverPalabras claves:Autores:Berrazueta M., Darío A. Rodríguez, Denisse Leines, Esteban Valencia, Henry P. Lema, Víctor Hugo Hidalgo DíazFuentes:scopusAeropropulsive evaluation of boundary layer ingestion for medium electric-powered uavs
Conference ObjectAbstract: The performance benefits of ingesting the boundary layer (BLI), in conjunction with the developmentPalabras claves:Autores:Darío A. Rodríguez, Edgar H. Cando, Esteban Valencia, Miguel A. Ayala, Stalyn Fabian Simbaña Caiza, Víctor H. Alulema, Víctor Hugo Hidalgo DíazFuentes:scopusExperimental performance assessment of an electric uav with an alternative distributed propulsion configuration implemented for wetland monitoring
Conference ObjectAbstract: Unmanned aerial vehicles (UAVs) have been recently adopted as an environmental monitoring tool due tPalabras claves:Autores:Alex F. Oña, Darío A. Rodríguez, Esteban Valencia, Miguel Angel Oña, Víctor Hugo Hidalgo DíazFuentes:scopusNovel 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:scopusParametric modeling for aerodynamic assessment of a fixed wing UAV implemented for site specific management
Conference ObjectAbstract: The aerodynamic characterization of a UAV during preliminary design brings several challenges, suchPalabras claves:Autores:Darío A. Rodríguez, Esteban Valencia, Víctor Hugo Hidalgo DíazFuentes:scopusPower management strategies for small electric fixed wing uavs employed in natural resources mapping
Conference ObjectAbstract: Small Electric fixed-wing unmanned Aerial Vehicles (SE-FW UAVs) constitute a very powerful tool forPalabras claves:Autores:Darío A. Rodríguez, Deyanira Valencia, Edgar H. Cando, Esteban Valencia, Iván D. Changoluisa, Johanna E. Nandar, Juan D. Hernández, Marcelo Pozo, Patricio Javier Cruz Davalos, Víctor H. AlulemaFuentes:scopusPropulsion sizing correlations for electrical and fuel powered unmanned aerial vehicles
ArticleAbstract: Despite the increasing demand of Unmanned Aerial Vehicles (UAVs) for a wide range of civil applicatiPalabras claves:Aircraft design, Battery technology, Electric propulsion, Internal combustion engines, Jet engines, Preliminary design, Unmanned aerial vehiclesAutores:Darío A. Rodríguez, Edgar H. Cando, Esteban Valencia, Víctor H. Alulema, Víctor Hugo Hidalgo DíazFuentes:scopusStatic aeroelastic approach based on Vortex lattice method and euler-bernoulli beam theory for structural analysis of fixed wing sUAS
ArticleAbstract: Unmanned Aerial Vehicles performing in the Andean Region (3000-5000 m.a.s.l) impose different operatPalabras claves:Andean Region, Static aeroelasticity, SUASAutores:Alexander F. Ramos, Darío A. Rodríguez, Esteban Valencia, Víctor H. AlulemaFuentes:scopus