Application of the DRGEP and Engagement Methods to Reduce the Reaction Mechanisms for Calculation of Chemically Non-Equilibrium Flows in Aircraft Engine Nozzles

Application of the DRGEP and Engagement Methods to Reduce the Reaction Mechanisms for Calculation of Chemically Non-Equilibrium Flows in Aircraft Engine Nozzles

The procedure of the reaction mechanism reduction including the DRGEP and engagement methods is considered and applied to the problem of calculating the non-equilibrium flows of propellant combustion products (kerosene + oxygen) in nozzles.

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Veröffentlicht in:Russian aeronautics 2018-10, Vol.61 (4), p.682-686
Hauptverfasser: Krioukov, V. G., Abdullin, A. L., Nikandrova, M. V., Safiullin, I. I.
Format: Artikel
Sprache:eng
Schlagworte:
Aircraft and Rocket Engine Theory
Aircraft engines
Automotive Engineering
Combustion products
Engineering
Kerosene
Mathematical analysis
Nozzles
Organic chemistry
Propellant combustion
Reaction mechanisms
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Beschreibung
Zusammenfassung:The procedure of the reaction mechanism reduction including the DRGEP and engagement methods is considered and applied to the problem of calculating the non-equilibrium flows of propellant combustion products (kerosene + oxygen) in nozzles.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799818040281