FIELD: aviation. SUBSTANCE: proposed flying vehicle has fuselage and two wings. Arranged in fuselage are gas-dynamic system and controllable gasdynamic flaps. Injector holes made in upper and lower parts of fuselage above and under outlet holes form two rows located along inner edge of each wing at the top and at the bottom relative to it. Control of gasdynamic flaps is effected by means of on-board computer. EFFECT: enhanced efficiency. 4 cl, 2 dwg
Authors
Dates
2003-05-27—Published
2002-01-29—Filed