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Gas dynamics and thrust in the exhaust system of a jet engine with an annular nozzle

Author:
V. A. Levin   N. E. Afonina   V. G. Gromov   G. D. Smekhov   A. N. Khmelevskii   V. V. Markov  


Journal:
Combustion, Explosion, and Shock Waves


Issue Date:
2012


Abstract(summary):

Results of a comprehensive numerical and experimental study of the dynamics of the flow of equilibrium combustion products of stoichiometric acetylene-air mixtures in the exhaust system of a jet engine with an annular nozzle are presented. Results of the numerical solution of unsteady Navier-Stokes equations for a chemically nonequilibrium model of a multispecies gas medium are reported. Experiments are performed in a hotshot aerodynamic setup. Thrust characteristics of the exhaust system of the jet engine are determined, and specific features of the structure of a steady flow formed there are found.


Page:
406-417


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