The technique of aerodynamic tests of models of fighters with imitation of engines of the power plant is presented. Verification of the developed technique is carried out by comparison of T-1 of the Kharkiv university of Air Powers of results received at a purge of model of the fighter aircraft MiG-29 in a wind tunnel with given natural experiment. Difference of the developed technique from known is introduction of the amendment on resistance of the long internal channel of motor-gondolas of model of the fighter aircraft.
wind tunnel, aerodynamic characteristics, model experiment, simulator, channel, engine
"Metodyka aerodynamichnykh vyprobuvan modelei vynyshchuvachiv z imitatsiieiu dvyhuniv" [Technique of aerodynamic tests of models of fighters with imitation of engines],
Science and Technology of the Air Force of Ukraine,