| 摘要 |
FIELD: aviation. ^ SUBSTANCE: proposed aircraft has fuselage, wing, main power plant with two turbo-jet engines 1, auxiliary power plant 2, fin assembly and side air intakes. Power plant 2 includes two supersonic turbo-jet engines 1 which are mounted in widened tail section of fuselage for placing fin assembly root in between them. Auxiliary power plant 2 is located at the bottom of center section of fuselage behind pilot cabin. Inlet openings of air intakes are made under wing and are bounded by fuselage in lower parts. Wing is provided with controllable slotted louvres in upper part of air intakes for air replenishment. Boundary layer drainage slots are made between upper edge of air intakes and lower surface of wing. ^ EFFECT: enhanced efficiency of multi-purpose supersonic aircraft. ^ 3 cl, 4 dwg |
