FIELD: transport.
SUBSTANCE: control method of flow of unpiloted aircraft includes outlet of working medium under pressure in nose part with density of less than 0.06 g/cm3, which contains dissociated hydrogen. In pulsating mode with frequency of 10 to 12000 Hz there formed around the fuselage is aerodynamic cone in the form of entropy layer in which energy of incoming flow is accumulated to be utilised in combustion chamber and in guide vane of power plant.
EFFECT: reducing aerodynamic resistance and heat load on the design with increase of speed and flight range.
1 dwg
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