Thesis
DISEÑO AERODINÁMICO DE UN PROTOTIPO DE VEHÍCULO AÉREO NO TRIPULADO (UAV)
Autor
ING. DELGADO ROMERO, VÍCTOR MANUEL
Institución
Resumen
This dissertation is centered in the aerodynamic study of an unmanned aerial vehicle
prototype, beginning with a concept that is sized in accordance with classical equations of the
aerodynamic; it is evaluated considering a low Reynolds number of 5 105.
During the design process the concept is improved up to achieve an aircraft e¢ cient and
stable aerodynamically.
The principal results obtained are total lift and drag coe¢ cients in function of fuselage
angle. These coe¢ cients are employed in the building of drag polar.