Параметрическое исследование взаимодействия частиц конденсированной фазы с высокоэнтальпийным потоком воздуха в прямоточной камере сгорания

17 / 18

Параметрическое исследование взаимодействия частиц конденсированной фазы…
Инженерный журнал: наука и инновации # 8·2017 17
Parametric study of condensed phase particles interaction
with a high-enthalpy air flow
in a co-current combustion chamber
© A.V. Voronetskiy 1, V.I Smolyaga2, K.Yu. Arefiev 1,
A.A Gusev1, M.A.Abramov1
1Bauman Moscow State Technical University, Moscow, 105005, Russia
2Joint-stock company Scientific-Production Association SPLAV, Tula, 300004, Russia
The article considers mathematical modeling working process problems in perspective
energy-power plants for intra-atmospheric aircraft using fuel based on high-metallized
energy-intensive compositions (VEK). The mathematical model developed and realized in
the specialized module allows us to adapt the software package ANSYS Fluent for simu-
lating a two-phase gas-dynamic flow taking into account the condensed BEC particles
combustion in a high-enthalpy air stream. The article gives the parametric calculations,
which result in obtaining some regularity in the particles combustion completeness coef-
ficient and its changing dependence on the ratio of components, two-phase mixing condi-
tions, and empirical constants in the combustion law. The article considers the cases of
particle feeding both from the combustion chamber wall and along the flow axis. The ob-
tained data can be used to refine the condensed particles combustion empirical laws, to
predict the physical and chemical processes completeness in real chambers and to devel-
op recommendations for improving the work process efficiency in advanced power-
generating plants.
Keywords: mathematical modeling, condensed fuel particles, air flow, mixture formation
scheme, empirical combustion law
REFERENCES
 Varenykh N.M., Shabunin A.I., Sarabev V.I., et al. Boepripasy i spetskhimiya —
Ammunition and special chemistry, 2013, no. 1, pp. 44–50.
 Bakulin V.N., Dubovkin N.F., Kotov V.N., Sorokin V.A., Frantskevich V.P.,
Yanovskiy L.S. Energoemkie goryuchie dlya aviatsionnykh i raketnykh
dvigateley [Energy-intensive fuels for aviation and rocket engine]. Moscow,
Fizmatlit Publ., 2009, 400 p.
 Kurth G., Bauer C., Hopfe N. Performance Assessment for a Throttlable Duct-
ed Rocket Powered Lower Tier Interceptor. 51st AIAA/SAE/ASEE. Proc. of
Joint Propulsion Conference, Propulsion and Energy Forum, USA, Orlando,
27–29 July 2015 (AIAA 2015-4234), pp. 6407–6423.
 Aleksandrov V.N., Bytskevich V.M., Verkholomov V.K., et al. Integralnye
pryamotochnye vozdushno-reaktivnye dvigateli na tverdykh toplivakh. Osnovy
teorii i rascheta [Integral ramjet air-jet engines on solid fuels. Fundamentals of
theory and calculation]. L.S. Yanovskiy, ed. Moscow, Akademkniga Publ.,
2006. 343 p.
 Averkov I.S., Aleksandrov V.Yu., Arefev K.Yu., Voronetskiy A.V., Guskov O.V.,
Prokhorov A.N., Yanovsky L.S. Teplofizika vysokikh temperatur — High Temper-
ature, 2016, no. 6, pp. 882–891.
 Voronetskiy A.V. Nauka i obrazovanie: ehlektronnoe nauchno-tekhnicheskoe
izdanie — Science and Education: Scientific Publication , 2016, no. 1. Avai-
lable at: (accessed May 15, 2017).