Table of Contents Table of Contents
Previous Page  18 / 19 Next Page
Information
Show Menu
Previous Page 18 / 19 Next Page
Page Background

А.В. Воронецкий, В.И. Крылов, К.Ю. Арефьев, А.А. Гусев

18

Инженерный журнал: наука и инновации

# 1·2017

The methodological aspects covering the development

of mathematical models of metal particles combustion in air

© A.V. Voronetskiy, V.I. Krilov,

K.Yu

. Aref’yev, A.A. Gusev

Bauman Moscow State Technical University, Moscow, 105005, Russia

The article deals with the combined computational and experimental approach for clari-

fying the empirical constants in the combustion law of the particles of powdered metal

fuel (PMF). A possibility of the method usage is demonstrated on modelling of flame

front propagation in a constant volume experimental stand. The paper considers a design

of the experimental stand and the methodology of the experiment. It also describes math-

ematical model used. A comparison of the calculated and experimental values of the

flame front speed for PMF gas suspensions is included. The possibility of applying this

combined computational and experimental approach to clarify the physical and mathe-

matical models to describe the ignition and combustion of two-phase reactive gas dynam-

ic flows is shown.

Keywords:

mathematical modeling, experimental research, metal particles combustion,

flame front, combustion chamber, combustion law

REFERENCES

[1]

Aleksandrov

V.Yu

., Aref’yev

K.Yu

., Prokhorov A.N., Fedotova K.V., Sha-

rov M.S., Yanovskiy L.S.

Izvestiya vysshikh uchebnykh zavedeniy

.

Mashi-

nostroenie — Proceedings of Higher Educational Institutions. Machine Build-

ing

, 2016, no. 2, pp. 65–75.

[2]

Obnosov B.V., Sorokin V.A., Yanovskiy L.S., Balyko Yu.P., Frantskevich V.P.,

Yagodnikov D.A., Zhivotov N.P., Surikov E.V., Sharov M.S., Tikhomirov M.A.

Konstruktsiya i proektirovanie kombinirovannykh raketnykh dvigateley na

tverdom toplive

[Construction and design of combined solid-fuel rocket engines].

Moscow, Bauman MSTU Publ., 2014, 279 p.

[3]

Kurziner R.I.

Reaktivnye dvigateli dlya bol'shikh sverkhzvukovykh skorostei

poleta

[Jet engines for high-supersonic speeds]. Moscow, Mashinostroenie

Publ., 1989, 263 p.

[4]

Demidov S.S., Malinin V.I., Bulbovich R.V.

Vestnik PNIPU. Aerokosmiche-

skaya technika

PNRPU Aerospace Engineering Bulletin

, 2014, no. 36,

pp. 119–130.

[5]

Voronetskii A.V.

Nauka i obrazovanie — Science and Education

, 2016, no. 1.

Available

at:

http://technomag.bmstu.ru/doc/830993.html

(accessed

18.08.2016).

[6]

Pohil P.F., Belyaev A.F., Frolov Yu.V.

Gorenie poroshkoobraznykh metallov v

aktivnykh sredakh

[Combustion of powder metals in active media]. Moscow,

Nauka, 1972, 294 p.

[7]

Kudryavtsev V.M., Sukhov A.V., Voronetskii A.V. Rasprostranenie fronta

khimicheskoy reaktsii v dvukhfaznom potoke [Spreading of chemical reaction

front in two-phase flow].

Visokotemperaturnye gazovye potoki, ikh poluchenie

i diagnostika

[High-temperature gas flows, their creation and diagnostics].

1987, vol. 4, pp. 66-69.

[8]

Shevchuk V.G., Goroshin S.V., Klyachko L.A.

Fizika goreniya i vzryva

Phys-

ics of combustion and explosion

, 1980, vol. 1, pp. 57–63.