Aerodynamic layout of a high-altitude long-endurance aircraft with twin fuselages, high rear wings and three surfaces
A technology of aerodynamic layout and long endurance, applied in aircraft, motor vehicles, transportation and packaging, etc., can solve problems such as adverse interference of rear wings, and achieve the effect of improving overall aerodynamic characteristics, increasing flight height, and improving aerodynamic characteristics.
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[0028] The present invention will be further described below in conjunction with the accompanying drawings.
[0029] In the aerodynamic layout of the aircraft of the present invention, the aircraft adopts a cylindrical cross-section double fuselage 1, a front wing 2 and a rear wing 3 of a larger aspect ratio, a V-shaped support tail 4, a horizontal tail 5 and a turbofan engine 6, such as figure 1 shown.
[0030] Such as figure 2 , image 3 As shown, the axes of the cylindrical cross-section twin fuselages 1 are parallel, including a left and right fuselage 101 and a right fuselage 102 that are left and right symmetrical; Between the quarter point and the third point of the long wingspan, preferably close to the third point. The aspect ratio of the front wing 2 and the rear wing 3 is greater than 7, depending on the specific situation, the larger the aspect ratio, the better.
[0031] Installed in the front half of the double fuselage 1, it is composed of the left end 201 ...
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