Positive-pressure flying aircraft

A positive-pressure flying aircraft comprising:

• a main body having a front end;
• a right body disposed at one side of the main body and having a front end;
• a left body disposed at the other side of the main body and having a front end, the front ends of the right and left bodies being behind the front end of the main body;
• a wing supported by the main body, the right body and the left body and having a front end that is behind the front ends of the right and left bodies, an air path being defined longitudinally of the aircraft by a bottom surface of the wing and inner side surfaces of the right and left bodies;
• a horizontal stabilizer;
• a thrusting device in a gap;
• a vertical fin in the middle of the horizontal stabilizer;
• a rudder at the rear end of the vertical fin;
• and
• an elevator at the rear end of the horizontal stabilizer,
• wherein one of the upper surface and the lower surface of the wing is flat, the other one of the upper surface and the lower surface of the wing has a positive camber, one of the upper surface and the lower surface of the horizontal stabilizer is flat, and the other one of the upper surface and the lower surface of the horizontal stabilizer has a positive camber, one of the upper surface of the wing and the upper surface of the horizontal stabilizer being flat, the other one of the upper surface of the wing and the upper surface of the horizontal stabilizer having a positive camber, the gap being formed between the wing and the horizontal stabilizer, and
• wherein the front end of each of the right body and the left body is formed as a hemisphere.