Listar por autor "Aguilar-Cabello, Jorge"
Mostrando ítems 1-9 de 9
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Active control of trailing vortices by synthetic jets in the axial direction near the wingtip.
Del-Pino-Peñas, Carlos Manuel
; Parras-Anguita, Luis; García-Ortiz, José Hermenegildo; Aguilar-Cabello, Jorge; Blanco-Rodríguez, Francisco José; Gutiérrez-Castillo, Paloma[et al.] (2024)
We applied an oscillating synthetic jet in the axial direction to a wingtip vortex and observed a decrease in its strength (active control, synthetic jets, wingtip vortex). -
DPIVSoft-OpenCL: a multicore CPU-GPU accelerated open source code for 2D Particle Image Velocimetry
Aguilar-Cabello, Jorge; Parras-Anguita, Luis; Del-Pino-Peñas, Carlos Manuel (Elsevier, 2022-11-21)
We present a translation of the original Matlab DPIVSoft code to a complete open source code implemented in Python, to perform Particle Image Velocimetry (PIV) in two-dimensions, in parallel, and with interrogation window ... -
Evaluación por competencias en asignatura troncal de Mecánica de Fluidos
Parras-Anguita, Luis; Aguilar-Cabello, Jorge; Blanco-Rodríguez, Francisco José; Gutiérrez-Castillo, Paloma; Hijano Pérez, Antonio Jesús; Olmo-Sánchez, María Isabel; Del-Pino-Peñas, Carlos Manuel; Serrano-Aguilera, Juan José[et al.] (Congreso Nacional de Ingeniería Mecánica, 2021)
Este trabajo presenta una propuesta de evaluación por competencias para una asignatura troncal de Mecánica de Fluidos. Se propone eliminar el examen final para la evaluación del aprendizaje por una evaluación continua ... -
Higher order dynamic mode decomposition of an experimental trailing vortex
Gutiérrez-Castillo, Paloma; Garrido-Martín, Manuel; Bölle, Tobias; García-Ortiz, José Hermenegildo; Aguilar-Cabello, Jorge; Del-Pino-Peñas, Carlos Manuel[et al.] (AIP, 2022-10-27)
The decay of trailing vortices is a fundamental problem in fluid mechanics and constitutes the basis of control applications that intend to alleviate the wake hazard. In order to progress, we use the recently developed ... -
Higher order dynamic mode decomposition to identify decay in trailing vortices
Gutiérrez-Castillo, Paloma; Garrido-Martín, Manuel; Bölle, Tobias; García Ortiz, José Hermenegildo; Aguilar-Cabello, Jorge; Del-Pino-Peñas, Carlos Manuel[et al.] (2022)
We conduct three-dimensional measurements of the velocity field using stereo PIV in the turbulent wake of a wing model based on a NACA0012 airfoil, for an angle of attack of 9 degrees, and Reynolds number 40000 up to 32 ... -
On the steady and unsteady aerodynamics of wing models at low Reynolds numbers for micro air vehicle applications
(UMA Editorial, 2021-12-14)Resumen tesis:In this thesis we have studied the stationary and non-stationary aerodynamic characteristics of wings at low Reynolds numbers commonly achieved in MAVS vehicles. The lift coefficient for a flat plate at low ... -
PIV measurements of the effect of pulsed blowing jet on a NACA0012 wing model
García Ortiz, José Hermenegildo; Aguilar-Cabello, Jorge; Guzmán Gómez, Alicia; Parras-Anguita, Luis; Del-Pino-Peñas, Carlos Manuel (Congress for the 19th Laser Symposium, 2018-07-16)
Wingtip vortices are present in taking off, and landing operations and their presence in airport runways must be reduced. To that end, several strategies have been considered in the last decades, being the active control ... -
Stability analysis of flow structures in hovering using robotic experiments and flow visualizations
Marín-Navarro, Alejandro; Aguilar-Cabello, Jorge; Parras-Anguita, Luis; Del-Pino-Peñas, Carlos Manuel (Lisbon Laser Symposium, 2018)
We investigate the kinematics and stability of hovering flight making use of a robotic experimental device that simulate the movement of insects or birds. We carried out this analysis based on the characterization of ... -
Theoretical parameters of trailing vortices versus aspect ratio of wing models
Aguilar-Cabello, Jorge; Jiménez-Rodríguez, Alberto; Parras-Anguita, Luis; Del-Pino-Peñas, Carlos Manuel (2019-07-18)
We perform 2D-PIV measurements to characterize trailing vortices in NACA0012 wing models for aspect ratios ranging between 1 and 2.5, and for chord-based Reynolds numbers from 7000 to 40000. Firstly, and regarding the ...