wing strut or leg of cylindrical section with our fairing it possesses a Cd = 0.06
The aerodynamic resistance of the
wing strut and leg of main floats with the fairing decreases of about 16
The fairing of the
wing strut and the leg of main floats allows to reach more elevated speed of flight, diminution of the consumption of
fuel, more elevated autonomies.
The planning of the models and of stamps has been effected to the computer.
The used material is the fiberglass.
The fabric of glass introduces a weight of 200
g/mqs; the used resin is type epoxy resin.
The finishing touch of the surface is realized with
The color is white.
The fiberglass allows a saving of weight and the necessary structural resistance required by the
includes a kit of assemblage to the wheel of the aircraft.
are equipped by a manual of assemblage.