Diseño conceptual y preliminar de una aeronave tipo Homebuilt de configuración Canard.

Abstract

This degree work, sought to apply the concept of Canard aircraft in the conceptual design and preliminary homebuilt aircraft a type. Based on the initial requirements and taking as guides the baseline, performing several studies with the purpose of obtaining the best results in performance, speed, range, range and height with respect to other aircraft of its kind. The concept of the wing with progressive arrow or forward sweep and its characteristics, being applied in an innovative way to an aircraft of this type, with the necessary arguments and documentary evidence on the improvements that are possible to obtain. Also considered the possibility of achieving an aerodynamic design that allowed to obtain a high performance and to be aesthetically more attractive the aircraft.