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Listar por palabra clave "Fixed wing"

Mostrando ítems 1-7 de 7

Computational Study of the Propeller Position Effects in Wing-Mounted, Distributed Electric Propulsion with Boundary Layer Ingestion in a 25 kg Remotely Piloted Aircraft

Serrano, J.R.; Tiseira, Andrés-Omar; García-Cuevas González, Luis Miguel; Varela-Martínez, Pau (MDPI AG, 2021-09)

[EN] Distributed electric propulsion and boundary layer ingestion are two attractive technologies to reduce the power consumption of fixed wing aircraft. Through careful distribution of the propulsive system elements, ...
Design, build and fly UAV

Ivars Martínez, Josep; Duineveld, Melvin; Martens, Jordy; Van der Horst, Maarten; Manders, Gijs (Universitat Politècnica de València, 2022-09-15)

[EN] The first objective of this project is to design an airplane that can fly statically stable and has a low enough stall speed to be hand launched. The design must also meet all the requirements as stated below. Also, ...
Diseño conceptual de un avión VTOL mediante uso de pila de combustible

Flors Bel, Carlos Jesús (Universitat Politècnica de València, 2023-11-07)

[ES] El trabajo trata de diseñar un avión conceptual partiendo de la base de ser un sistema VTOL pero el cual tiene una planta propulsiva mediante el uso de pila de combustible. En el diseño se busca distintos tipos de ...
Diseño y Construcción de Aeronave Demostrador No Tripulada para Estudio de Alas Experimentales

Flors Bel, Carlos Jesús (Universitat Politècnica de València, 2021-10-19)

[ES] El presente trabajo consiste en el diseño, cálculo preliminar y construcción de una aeronave demostrador no tripulada como plataforma para el futuro estudio de diversas alas rectangulares con diversas geometrías. La ...
Motion Equations and Attitude Control in the Vertical Flight of a VTOL Bi-Rotor UAV: Part 2

Musoles, Jose Luis; Garcia-Nieto, Sergio; Simarro Fernández, Raúl; Ramos Fernández, César (MDPI AG, 2024-07)

[EN] This paper gathers the dynamical modeling of an unmanned aircraft and the design and simulation of the control system, allowing it to perform a Vertical Take-Off (VTOL) maneuver, a fixed-wing (FW) flight and a transition ...
Optimal aerodynamic conceptual design of the MERMOZ hydrogen powered UAV

Millet, Theo Augustin (Universitat Politècnica de València, 2022-09-28)

[EN] The MERMOZ drone is an electrically powered drone based on the use of a battery of hydrogen that allows long-range missions (up to 3,000 km) to be carried out without CO2 emissions. The Optimization of the aerodynamic ...
Propeller Position Effects over the Pressure and Friction Coefficients over the Wing of an UAV with Distributed Electric Propulsion: A Proper Orthogonal Decomposition Analysis

Serrano, J.R.; García-Cuevas González, Luis Miguel; Bares-Moreno, Pau; Varela-Martínez, Pau (MDPI AG, 2022-02)

[EN] New propulsive architectures, with high interactions with the aerodynamic performance of the platform, are an attractive option for reducing the power consumption, increasing the resilience, reducing the noise and ...