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Vol 21, No 2 (2022)

Influence of pad geometry and method of oil supply on the thermal state of GTE rotor tilting-pad journal bearing

Parovay E.F.

(Rus)

Vol 21, No 4 (2022)

Methodology for thermal calculation of the heat exchanger for cooling the air at the intake of the aerospace plane engine compressor

Panchenko S.L., Gras’ko T.V.

(Rus)

Vol 20, No 3 (2021)

Development of a methodology for calculating the working process of a small-size two-stroke internal combustion engine

Biryuk V.V., Gorshkalev A.A., Zakharov M.O., Larin V.L.

(Rus)

Vol 18, No 3 (2019)

Mathematical model for calculating the mass of a heat exchanger in problems of optimizing the parameters of the working process of aircraft gas turbine engines

Kuz'michev V.S., Omar H., Tkachenko A.Y., Bobrik A.A.

(Rus)

Vol 12, No 3-1 (2013): Vestnik SSAU

System of pressurization of the fuel tank of a launch vehicle using the heat of generator gas

Biryuk V.V., Smorodin A.V., Shepelev A.I., Onoprienko D.A.

(Rus)

Vol 19, No 4 (2020)

The effect of heat recovery on the optimal values of helicopter turboshaft engine parameters

Omar H.H., Kuz'michev V.S., Zagrebelnyi A.O., Grigoriev V.A.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

Features of calculation of hydraulic characteristics of capillary spray jets of is liquid-stnyh rocket engines of small pull-rod

1 1., 1 1., 1 1.

(Rus)

Vol 10, No 5 (2011)

Analysis of the properties of water condensate obtained from heat engine exhaust yases

Knysh Y.A., Uglanov D.A.

(Rus)

Vol 11, No 3-3 (2012): Special Issue

The calculation of optimum worker frequencies of the thermoacoustic electric generator with including ready electrodynamic unit and given load

Vorotnikov G.V., Kryuchkov A.N.

(Rus)

Vol 9, No 1 (2010)

Influence of the loading parameter on the efficiency ofa three-stage turbine of turbojet bypass engine

1 1., 1 1.

(Rus)

Vol 14, No 1 (2015)

Vortex cleaning of fuel tank pressurant gas

Biryuk V.V., Shimanov A.A., Onoprienko D.A., Smorodin A.V., Shepelev A.I.

(Rus)

Vol 13, No 1 (2014)

Analysis of nonstationary thermal state of a low-thrust liquid rocket engine taking into account injection, evaporation and combustion of liquid fuel droplets

Vorobiev A.G., Borovik I.N., Ha S.

(Rus)

Vol 8, No 3-1 (2009): Special Issue

Research of a seal work as an element of the air engine support

Vinogradov A.S., Rempel A.P.

(Rus)

Vol 10, No 3-4 (2011): Special Issue

The determination of the thermoacoustic generator aspect from electrodynamic unit features by the parametric-studies

Vorotnikov G.V., Kruchkov A.N., Zynovyev E.A.

(Rus)

Vol 9, No 4 (2010)

Parametric analysis of thermoacoustic travelling-wave engine operation with external heat application

Dovgyallo A.I., Zynovyev Y.A., Vorotnikov G.V.

(Rus)

Vol 14, No 2 (2015)

Strength analysis of internal combustion engine elements by using ANSYS with taking into account heat processes in the combustion chamber

Biryuk V.V., Gorshkalev A.A., Kayukov S.S., Saigakov E.A.

(Rus)

Vol 13, No 5-2 (2014): Special Issue

Automated thermovacuum firing test facility for testing and research of workflow in low-thrust rocket engine on hypergolic propellants

Galperin R.N., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.

(Rus)

Vol 13, No 5-1 (2014): Special Issue

The influence of the shuttle effect on the intensification of heat losses in a Stirling engine

Savchenko V.A., Stolyarov S.P.

(Rus)

Vol 11, No 3-3 (2012): Special Issue

The modeling of the thermoacoustic electric generator by quadrupole approximation approach

Vorotnikov G.V.

(Rus)

1 - 19 of 19 Items

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