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

Experimental verification of the possibility of improving the liquid propelant rocket engine performance for the “Vega” launcher upper stage

Kovalenko A.N., Pereverzev V.G., Marchan R.A., Blishun Y.V.

(Rus)

Vol 22, No 1 (2023)

Results of conjugate modeling and analysis of the thermal state of a high-pressure turbine blade

Matveev V.N., Melnikov S.A., Popov G.M., Zubanov V.M., Kudryashov I.A., Shcherban A.I.

(Rus)

Vol 23, No 3 (2024)

Development and research testing of a low thrust on gaseous-propellant rocket engine chamber

Musteikis A.I., Levikhin A.A., Kolosenok S.V.

(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 21, No 2 (2022)

3D investigation of heat exchange and hydrodynamics of high pressure turbine nozzle block platforms with different cooling schemes

Gorelov Y.G., Ananyev V.V., Zolotuhina D.A.

(Rus)

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

Analisys of experimental combustion chambers fire tests for LRE with cooling by liquid oxigen for "DM" type booster

Smolentsev A.A., Strizhenko P.P.

(Rus)

Vol 13, No 1 (2014)

Analysis of nonstationary thermal state of low-thrust liquid rocket engine with high-concentration hydrogen peroxide and kerosene propellant with film cooling

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

(Rus)

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

Particularity of thermal condition computation oF LRE with cooling by liquid oxygen

1 1.

(Rus)

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

Analysis of the thermal state of aircraft engine supports

Vinogradov A.S., Badykov R.R., Fedorchenko D.G.

(Rus)

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

Increase in thermal efficiency of the conditioned clothing

Savchenko N.V.

(Rus)

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

Improving the efficiency of gas turbines by regenerating heat

Kulagin V.V., Sokolov M.A.

(Rus)

Vol 11, No 3-1 (2012): Special Issue

To the question of cooling power components of radio-electronic equipment by impinging freon jets

Lopatin A.A., Gortyshov Y.F.

(Rus)

Vol 12, No 3-2 (2013): Vestnik SSAU

3d calculation of a multiport low-emission combustor cooling system

Moreva I.S., Vasilyuk D.K., Kirichenko R.Y.

(Rus)

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

Preliminary study of principles of effective efficiency change of turboshaft engines of various schemes with heat recovery and intermediate cooling of working medium

Sokolov M.A., Kuzmichev V.S., Kulagin V.V., Krupenich I.N., Tkachenko A.Y.

(Rus)

Vol 13, No 2 (2014)

Automated selection of cooling system for radio electronic design of thermophysical

Goryachev N.V., Trusov V.A., Yurkov N.K.

(Rus)

1 - 15 of 15 Items

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