Listar por autor "Durán-Venegas, Eduardo"
Mostrando ítems 1-5 de 5
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Aerodynamic forces and wake structure on a 2D model of a vehicle in ground effect
Solís-García, Pedro; Zerzeri, Khaled; Nouailli, Mariem; Parras-Anguita, Luis
; Durán-Venegas, Eduardo (2023)
In this research we perform numerical simulations and wind tunnel experiments of a D-shaped bluff body. Different flow conditions and ground-body distances are considered to analyse the ground effect on aerodynamic forces ... -
Analysis of lift coefficient and trailing vortices properties at low Reynolds number with spanwise deformation.
Solís-García, Pedro; Garrido-Martín, Manuel; Durán-Venegas, Eduardo; Gutiérrez-Castillo, Paloma; Del-Pino-Peñas, Carlos Manuel (2024)
Se ha estudiado experimentalmente qué efecto tiene la deformación longitudinal en alas sobre su coeficiente de sustentación y los vórtices de punta de ala. -
Cavity flow induced by a flexible membrane in an oscillatory channel flow: case study of syringomyelia.
(2023)In this work, we study the flow inside a Syringomyelia, modelled by a cavity separated from a channel with an elastic membrane. The oscillatory flow of the channel is transmitted to the cavity through the deformation of ... -
Experimental passive control of the Ahmed body without ground effect using deflectors at a low Reynolds number.
Solís-García, Pedro; Santiago, José Antonio; Durán-Venegas, Eduardo; Del-Pino-Peñas, Carlos Manuel (2024)
Hemos realizado una investigación experimental sobre el efecto de diferentes ángulos de deflectores en los coeficientes de arrastre y sustentación de un cuerpo Ahmed sin efecto suelo. Nuestros hallazgos muestran que el ... -
On the effect of deformation in a wing model on the correlation of the lift slope
Gutiérrez-Castillo, Paloma; Durán-Venegas, Eduardo; Konovalov-Shishov, Nikita; Del-Pino-Peñas, Carlos Manuel (2023)
Deformed wing models with a NACA0012 airfoil are analyzed experimentally in a wind tunnel at the University of Malaga. Measurements show the influence of the level of the deformation on the lift coefficient and, therefore, ...