| 摘要 |
PURPOSE: A glider is provided to improve stability and directionality by using variable wings and circular wings. CONSTITUTION: A glider comprises a ring segment(10), a wing portion(20), and a tail area(30). The ring segment has a circular cross-section. The ring segment is formed thicker than the wing portion. The ring segment is formed thicker towards center direction than the wing portion side. The wing portion is extended rearward from the circumference of the ring segment to the axial direction. The wing portion is cut in order to have downward slope towards tail area from a side look. The tail area is included in rear end of the wing portion. The tail area is formed into 2 three angle end parts which are symmetrical. |
