- -

On the Analysis and Design of Series Hybrid Distributed Electric Propulsion with Boundary Layer Ingestion of Remotely Piloted Aircraft

RiuNet: Institutional repository of the Polithecnic University of Valencia

Share/Send to

Cited by

Statistics

  • Estadisticas de Uso

On the Analysis and Design of Series Hybrid Distributed Electric Propulsion with Boundary Layer Ingestion of Remotely Piloted Aircraft

Show full item record

Varela Martínez, P. (2023). On the Analysis and Design of Series Hybrid Distributed Electric Propulsion with Boundary Layer Ingestion of Remotely Piloted Aircraft [Tesis doctoral]. Universitat Politècnica de València. https://doi.org/10.4995/Thesis/10251/192805

Por favor, use este identificador para citar o enlazar este ítem: http://hdl.handle.net/10251/192805

Files in this item

Item Metadata

Title: On the Analysis and Design of Series Hybrid Distributed Electric Propulsion with Boundary Layer Ingestion of Remotely Piloted Aircraft
Author: Varela Martínez, Pau
Director(s): García-Cuevas González, Luis Miguel
UPV Unit: Universitat Politècnica de València. Departamento de Máquinas y Motores Térmicos - Departament de Màquines i Motors Tèrmics
Read date / Event date:
2023-03-14
Issued date:
Abstract:
[ES] En el presente trabajo se explora posibles soluciones a dos hechos correlacionados que podrían comprometer hasta cierto punto nuestro futuro. Por un lado, el crecimiento de la flota de aeronaves pequeñas en los ...[+]


[CA] En aquest treball s'exploren possibles solucions a dos fets correlacionats que podrien comprometre d'alguna manera el nostre futur. Per un costat, el creixement de la flota d'aeronaus de xicoteta dimensió en el ...[+]


[EN] The present work explores possible solutions to two correlated events that could compromise our future to some extent. On the one hand, the growth of the fleet of small aircraft in the coming years, whether manned ...[+]
Subjects: Capa límite , Propulsión eléctrica distribuida , Integración fuselaje propulsión , Sistemas híbridos , Vehículo aéreo no tripulado (VANT) , Diseño de aeronaves , Airframe propulsion integration , Distributed electric propulsion , Boundary layer ingestion , Hybrid system , Unmanned aerial vehicle , Aircraft design
Copyrigths: Reserva de todos los derechos
DOI: 10.4995/Thesis/10251/192805
Publisher:
Universitat Politècnica de València
Project ID:
info:eu-repo/grantAgreement/UPV//PAID-02-2020
Thanks:
The respondent would like to acknowledge the financial support received through contract FPI-UPV PREDOCFD/19 of Subprograma 2 of Universitat Politècnica de València
Type: Tesis doctoral

recommendations

 

This item appears in the following Collection(s)

Show full item record