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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 10, No 6 (2011)

Theoretical and experimental investigation of the photographic reconnaissance plane instrument bay thermal state

Nikolayev V.N.

(Rus)

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

Research of the possibility of thermal conditions LREST using an infrared thermal imaging system

Ryzhkov V.V., Silyutin M.V.

(Rus)

Vol 10, No 1 (2011)

Theoretical and experimental analysis of the thermal state of transport aircraft compartments thermal state

Nikolayev V.N.

(Rus)

Vol 10, No 3-1 (2011): Special Issue

Estimate of key parameters of a gas turbine engines with application of the modelling procedure of the equilibrium state of homogeneous mixture of hydrocarbon fuel combustion products

Boldyrev O.I., Gorynov I.M.

(Rus)

Vol 14, No 3 (2014)

Development of a low-emission bifuel combustion chamber

Bubentsov A.V., Vasiluk D.K., Golubev P.A., Kirichenko R.E., Tashkinov V.A., Shoshin V.B.

(Rus)

Vol 10, No 3-1 (2011): Special Issue

Experimental researches of possible low-thrust rocket adaptation developed by FSUE R&DIME for bipropellant MON-3+MMH providing tolerable thermal state thrusters

Beshenev Y.A., Buldashev S.A., Kazankin F.A., Lemskiy N.V., Semkin Y.V.

(Rus)

Vol 11, No 5-2 (2012): Special Issue

Parameters study in the electrothermal and jet protection of the airliner cockpit windows from fogging

Nikolayev V.N.

(Rus)

Vol 13, No 5-3 (2014): Special Issue

Results of experimental studies of parameters of low-thrust rocket engines operating on gaseous oxygen-hydrogen fuel

Ageenko Y.I., Lapshin E.A., Morozov I.I., Pegin I.V., Ryzhkov V.V.

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

Automated generation of structural members of a spacecraft thermal model

Kulikov D.S., Shatin A.A., Velmisov I.G.

(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)

1 - 12 of 12 Items

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