Экспериментальное исследование теплогидравлических характеристик трактов охлаждения камер сгорания с предельными параметрами оребрения энергосиловых установок

12 / 13

В.П. Александренков, Н.Н. Зубков, Д.А. Ягодников, Н.Я. Ирьянов, А.В. Сухов
12 Инженерный журнал: наука и инновации # 10·2016
Experimental study of thermal-hydraulic characteristics
of combustion chamber cooling channels
with critical propulsion plant ribbing parameters
© V.P. Aleksandrenkov, N.N. Zubkov, D.A. Yagodnikov,
Iryanov, A.V. Sukhov
Bauman Moscow State Technical University, Moscow, 105005, Russia
The article presents results of an experimental investigation studying thermal-hydraulic
characteristics of combustion chamber cooling channels found in thermal propulsion
plants characterised by a critically high ribbing level generated via deformational cut-
ting technique. We show that these channels are operationally efficient when it comes to
cooling high-temperature propulsion plant structures and provide reliable thermal
shielding for said structures even in the case of film boil occurring in the coolant.
Keywords: circular cooling channel, combustion chamber ribbing, deformational cutting,
rotational flow, thermal-hydraulic characteristics.
REFERENCES
[1] Pelevin F.V., Ponomarev A.V., Semenov Izvestiya vysshikh uchebnykh
zavedeniy. Mashinostroenie — Proceedings of Higher Educational Institutions.
Маchine Building , 2015, no. 66, pp. 74–81.
[2] Zubkov N.N. Novosti teplosnabzheniya — Heat Supply News, 2005, no. 4,
pp. 51–53.
[3] Zoubkov N.N. (RU), Ovtchinnikov A.I. (RU). Method and apparatus producing
a surface with alternating ridges and depressions. Pat. 5775187 USA, Int. Cl.
B23B 17/00, no. 545640, 1998.
[4] Popov I.A., Shchelchkov A.V., Zubkov N.N., Ley R.A., Gortyshov Yu.F.
Izvestiya vysshikh uchebnykh zavedeniy. Aviatsionnaya tekhnika — Russian
Aeronautics , 2014, no. 4, pp. 49–53.
[5] Pelevin F.V., Avraamov N.I., Orlin S.A., Sintsov A.L. Inzhenernyy zhurnal:
nauka i innovatsii — Engineering Journal: Science and Innovation , 2013, no. 4.
DOI: 10.18698/2308-6033-2013-4-698
[6] Yagodnikov D.A., Antonov Yu.V., Vorozheeva O.A., Masalskiy N.L., Novikov
A.O., Chertkov K.O. Inzhenernyy vestnik — Engineering Bulletin, 2014, no. 10.
Available at:
[7] Trusov B.G. Inzhenernyy zhurnal: nauka i innovatsii — Engineering Journal:
Science and Innovation, 2012, no. 1, pp. 21.
DOI: 10.18698/2308-6033-2012-1-31
[8] Kudryavtsev V.M., ed. Osnovy teorii i rascheta zhidkostnykh raketnykh
dvigateley [Foundations of liquid rocket engine theory and parameter
calculation]. In 2 vols. Vol. 2. Moscow, Vysshaya Shkola Publ., 1993, 703 p.
[9] Grigorev E.Z., Meylikhov I.S., ed. Fizicheskie velichiny [Physical quantities].
Moscow, Energoatomizdat Publ., 1991, 1000 p.
Aleksandrenkov V.P. , Cand. Sci. (Eng.), Assoc. Professor, Department of Rocket En-
gines, Bauman Moscow State Technical University. e-mail:
Zubkov N.N. , Dr. Sci. (Eng.), Professor, Department of Tooling Equipment and Tech-
nologies, Bauman Moscow State Technical University. e-mail: