| 摘要 |
FIELD: aviation. SUBSTANCE: wing has profile in form of isosceles triangle. Lower and upper generatrices (1,2) of wing lie in one plane with lateral sides of isosceles triangle of wing profile. Wing is additionally provided with rear surface (6) which lies in plane with base of isosceles triangle of wing profile and upper and lower edges (5,4) of wing which pass through angles at base of isosceles triangle of wing profile. Leading edge is formed by vertices of isosceles triangle of wing profile. Wing is secured in flying vehicle for performing free self-excited oscillations in flight. EFFECT: enhanced lateral dynamic stability. 5 dwg |
