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  5. The research of features of air intake in the rocket-based combined engine

The research of features of air intake in the rocket-based combined engine

M.А. Katrenko, А.Т. Kudrevatykh
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Results of theoretical researches of air intake in a rocket-basedt combined engine was present. Models of air inlet in the drive was consider at different number of air inlets and a variable corner of an air passage. Simulation of working process in a rocket-based combined engine are execute by a path of the solution of a set of equations of the Navier-Stokes describe flow of viscous compressible gas, a method of final volumes. Adequacy of computational models are show.
Keywords: flow of gas, air inlet, speed, consumption, mixture, nozzle