INTEGRAL AERODYNAMIC CONFIGURATION AIRCRAFT

摘要

FIELD: aviation. SUBSTANCE: center fuselage is smoothly engageable with swept wing panels, nose and tail fuselages. Tail fuselage carries port and starboard fins with rudders. Each fin or each rudder is set at acute angle in neutral position. Vertex of angle is directed backward relative to nose fuselage. Rudder angle for each rudder ranges form 1.5 to 2.5 deg. Such position of vertical tail unit reduces loads acting on fins. EFFECT: enhanced efficiency. 2 cl, 3 dwg