Simulation of a Rocket Engine Nozzle Discharge Coefficient |
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| Authors: | A. N. Sabirzyanov A. I. Glazunov A. N. Kirillova K. S. Titov |
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| Affiliation: | 1.Tupolev Kazan National Research Technical University,Kazan,Russia |
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| Abstract: | Multiparameter studies of the discharge coefficient dependence on the nozzle geometry and the presence of a condensed phase in combustion products were performed. The simulation results obtained satisfactorily agree with the well-known generalized data. The modern computational fluid dynamics methods were shown to be able to refine the generalized empirical relations. |
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