[ES] Proyecto realizado en movilidad en Bucarest. Los objetivos son: - Análisis CFD 2D para mejorar la configuración de un perfil aerodinámico con dispositivos hipersustentadores pasivos de borde de ataque y de salida para despegue. Para ello se emplea el software CONVERGE CFD. - Análisis CFD 3D de un ala con el perfil anterior equipado con los dispositivos hipersustentadores. Para ello se emplea el software FlightStream.[EN] Project carried out in mobility in Bucharest. The objectives are: - 2D CFD analysis to improve an airfoil configuration with passive high-lift leading and trailing edge devices for take-off. CONVERGE CFD software is used for this purpose. - 3D CFD analysis of a wing with the airfoil equipped with the chosen high-...
[ES] Este trabajo se centra en el estudio de la aerodinámica del dron Valaq 120 de la empresa UAV Wo...
[EN] This document shall detail all the processes followed for designing, calculating, analyzing an...
The development of this project is oriented towards the study of force coefficients and flow struct...
This thesis provides an study of the flow around a McDonnell Douglas 30P30N with an Active Flow Cont...
Boundary layer control is a very important subject of investigation in fluid mechanics. The inventi...
RESUMEN: En el presente proyecto de fin de grado, se pretende abordar el estudio aerodinámico de var...
[ES] El objetivo principal del presente trabajo de final de grado es analizar la influencia de las s...
Computational Fluid Dynamics (CFD) found its way into aircraft design starting with the important co...
This paper presents an aerodynamic optimization chain whose purpose is to find the optimal High Lift...
Airfoil can be defined as a body shape so that lift can be generated as fluid flow through it. The s...
Tez (Yüksek Lisans) -- İstanbul Teknik Üniversitesi, Fen Bilimleri Enstitüsü, 2004Thesis (M.Sc.) -- ...
En la presente investigación se estudió el efecto de incorporar protuberancias en el borde de ataque...
Given the importance of fuel reduction in the aeronautical industry, for both economic and environm...
A wingsail is a solid symmetrical aerofoil section which creates thrust in the samemanner as a conve...
The effect of suddenly deffecting a trailing-edge flap on an airfoil is studied using a validated, t...
[ES] Este trabajo se centra en el estudio de la aerodinámica del dron Valaq 120 de la empresa UAV Wo...
[EN] This document shall detail all the processes followed for designing, calculating, analyzing an...
The development of this project is oriented towards the study of force coefficients and flow struct...
This thesis provides an study of the flow around a McDonnell Douglas 30P30N with an Active Flow Cont...
Boundary layer control is a very important subject of investigation in fluid mechanics. The inventi...
RESUMEN: En el presente proyecto de fin de grado, se pretende abordar el estudio aerodinámico de var...
[ES] El objetivo principal del presente trabajo de final de grado es analizar la influencia de las s...
Computational Fluid Dynamics (CFD) found its way into aircraft design starting with the important co...
This paper presents an aerodynamic optimization chain whose purpose is to find the optimal High Lift...
Airfoil can be defined as a body shape so that lift can be generated as fluid flow through it. The s...
Tez (Yüksek Lisans) -- İstanbul Teknik Üniversitesi, Fen Bilimleri Enstitüsü, 2004Thesis (M.Sc.) -- ...
En la presente investigación se estudió el efecto de incorporar protuberancias en el borde de ataque...
Given the importance of fuel reduction in the aeronautical industry, for both economic and environm...
A wingsail is a solid symmetrical aerofoil section which creates thrust in the samemanner as a conve...
The effect of suddenly deffecting a trailing-edge flap on an airfoil is studied using a validated, t...
[ES] Este trabajo se centra en el estudio de la aerodinámica del dron Valaq 120 de la empresa UAV Wo...
[EN] This document shall detail all the processes followed for designing, calculating, analyzing an...
The development of this project is oriented towards the study of force coefficients and flow struct...