FIELD: jet engines of flying vehicles. SUBSTANCE: method consists in accelerating flow in jet engine which includes combustion chamber and nozzle fitted with tip having definite sizes protected by invention. Acceleration of flow is achieved through constriction of this flow in its subsonic part and widening in supersonic part. Asymmetry of flow is formed in nozzle and nozzle proper or part of it is deflected through angle α = ±arctgFy/Fx whose magnitude depends on Fy,Fx.. EFFECT: enhanced efficiency. 3 cl, 3 dwg
Authors
Dates
1998-01-27—Published
1995-09-07—Filed