Ideal aircraft. The present invention relates to the field tu00eacnico aeronautical, more specifically to an aircraft consisting of an innovative profile, or "fuselage" Aerodynamics (1), which allows a flight faster and with less fuel consumption.These advantages are possible thanks to the reduction of aerodynamic drag by sucking the air in the frontal area of the aircraft (a) for the propulsion motors (turbine) (c), that are within its fuselage on its back.And that creates a region of low density by the propulsion that is moved through the internal aerodynamic duct (2) and (3) to the frontal areas of the aircraft, taking advantage of the low air density, and thus its resistance.
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