METHOD OF DETERMINING THRUST IN FLIGHT OF BYPASS TURBOJET ENGINE WITH MIXING OF FLOWS

摘要

FIELD: engines.SUBSTANCE: invention relates to control of turbojet bypass engine with mixing of flows TCTREand TCTREwith afterburner TURBOFANSand enables to determine thrust in flight with high accuracy with account of real gas flow from jet nozzle.EFFECT: as per measurements of flight information parameters are measured gas at jet nozzle exit, at which the output impulse of the nozzle and actual engine thrust is determined as function of R =ƒ(P, t , V, n, p , p , F, F).1 cl