Email this article Application of the DRGEP and Engagement Methods to Reduce the Reaction Mechanisms for Calculation of Chemically Non-Equilibrium Flows in Aircraft Engine Nozzles
- Authors: Krioukov V.G.1, Abdullin A.L.1, Nikandrova M.V.1, Safiullin I.I.1
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Affiliations:
- Tupolev Kazan National Research Technical University
- Issue: Vol 61, No 4 (2018)
- Pages: 682-686
- Section: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230782
- DOI: https://doi.org/10.3103/S1068799818040281
- ID: 230782
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Abstract
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.
About the authors
V. G. Krioukov
Tupolev Kazan National Research Technical University
Email: kazan711@yandex.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111
A. L. Abdullin
Tupolev Kazan National Research Technical University
Email: kazan711@yandex.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111
M. V. Nikandrova
Tupolev Kazan National Research Technical University
Email: kazan711@yandex.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111
I. I. Safiullin
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: kazan711@yandex.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111
