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

M.А. Katrenko, А.Т. Kudrevatykh
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Description: 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

Reference:
Katrenko, M.A. and Kudrevatykh, A.T. (2016), “Issledovanie osobennostei podvoda vozdukha v kombinirovannom raketno-priamotochnom dvigatele” [The research of features of air intake in the rocket-based combined engine], Scientific Works of Kharkiv National Air Force University, Vol. 3(48), pp. 67-70.