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Distributed Electric Propulsion

dc.rights.licenseAll rights reserved
dc.contributor.advisorPertierra García, José R.
dc.contributor.authorMorales, Ángel
dc.contributor.authorTorres Rivera, Aníbal
dc.date.accessioned2019-11-11T16:35:00Z
dc.date.available2019-11-11T16:35:00Z
dc.date.issued2019-08-19
dc.identifier.urihttp://hdl.handle.net/20.500.12475/112
dc.descriptionFinal Research Poster for the Undergraduate Research Program for Honor Students HSI STEM Grant.
dc.description.abstractThis investigation focused on predicting aerodynamic improvements obtained when air is blown over a wing by six propellers distributed equally along the wing’s span The purpose was to validate a method to implement Distributed Electric Propulsion and quantify its impact during conceptual aircraft designen_US
dc.description.sponsorshipThis research project was supported by the Title V STEM Grant “Bridges to STEM Success” P 0031 C 160141
dc.language.isoenen_US
dc.publisherPolytechnic University of Puerto Ricoen_US
dc.relation.ispartofMechanical Engineering Program
dc.relation.ispartofseriesUndergraduate Research Program For Honor Students HSI STEM Grant 2018-2019
dc.relation.haspartSan Juan Campus
dc.subject.lcshAerodynamics
dc.subject.lcshPropulsion systems
dc.subject.lcshPropellers, Aerial
dc.subject.lcshVortex theory (Astrophysics)
dc.subject.lcshAirplanes--Wings
dc.subject.lcshPolytechnic University of Puerto Rico--Undergraduates--Posters
dc.titleDistributed Electric Propulsionen_US
dc.typePosteren_US
dc.rights.holderPolytechnic University ff Puerto Rico, Undergraduate Research Program For Honor Students HSI STEM Grant


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