| 摘要 |
FIELD: aviation. SUBSTANCE: wing has aerodynamic members symmetrical to each other in mirror image and smoothly engageable with wing. Each aerodynamic member is mounted at angle relative to wing plane and has sweep forward and sweep back form and unsymmetrical profile mounted at definite angle of attack. Provided over leading and trailing edges at height of aerodynamic element at definite distance is break where triangular profiled element at definite sweep by leading edge is mounted. EFFECT: enhanced efficiency of wing. 6 cl, 39 dwg |
