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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 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 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 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 11, No 2 (2012)

Mathematical modeling of heat exchange on air cooling of a number of aluminum ingots

Gorshenin A.S.

(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 12, No 2 (2013)

Agreement between criterial equations of heat transfer in the process of cooling aluminium ingots and experimental data

Gorshenin A.S., Krivosheev V.E.

(Rus)

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

Issues of evolution of rotor piston engines’ subject abroad and in Russia

Kocherov E.P., Kononov V.A., Okorochkov V.V., Okorochkova V.M., Ivanova K.P.

(Rus)

Vol 13, No 5-4 (2014): Special Issue

Experience in the development of 11Д58MФ liquid rocket engines

Smolentsev A.A.

(Rus)

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

Numerical investigation of phisical processes in cooling jacket of thrust chamber of LOx – LH2 LRE using 3D computer simulation methods

Yakub P.A., Gumennyy A.V.

(Rus)

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

Selection of new heat-resistant nickel alloys for advanced aviation engines

1 1., 1 1., 1 1., 1 1., 1 1.

(Rus)

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

Preliminary tests of tank with cryogenic charging for onboard throttle system of cooling

Dovgjallo A.I., Sarmin D.V., Uglanov D.A.

(Rus)

Vol 13, No 5-4 (2014): Special Issue

Mathematical modeling and investigation of the process of thermal theatment of aluminum ingots on the basis of regulated convective heat transfer

Gorshenin A.S., Krivosheev V.E.

(Rus)

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

The analyze of work of throttle cooling system’s microheat exchanger, wich uses nitrogen with nearly critical parameters

1 1., 1 1., 1 1., 1 1.

(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 5-3 (2014): Special Issue

Significance and directions of development of rotary piston area of research

Okorochkov V.V., Okorochkova V.M., Shafranov V.V.

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

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

1 1.

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

Thermal state of combustor can elements

Grechishnikov O.V., Ostapets I.I., Roslyakov A.D., Tsybizov Y.I.

(Rus)

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

Heat-pipes’ application for cooling of communications-electronics equipment

Biryuk V.V., Kitaev A.I.

(Rus)

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

Internal combustion engine some cooling system components detailed calculation

Kolomin I.V., Ajukov A.A., Birjuk V.V.

(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 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)

Vol 19, No 1 (2020)

Mathematical model of the “tank – nozzle” cooling system

Shalay V.V., Shcherban K.V.

(Rus)

Vol 10, No 3-2 (2011): Special Issue

Methodology of optimization of parameter of matching the combustion chamber and turbine joint operation

Grigoriev A.V., Golubchikov P.P., Ilushin M.Y., Rudakov O.A., Solovieva A.V.

(Rus)

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

Increase in thermal efficiency of the conditioned clothing

Savchenko N.V.

(Rus)

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

Investigation of thermal conditions nozzle blades with a cyclone-vortex cooling system

Veretennikov S.V., Khasanov S.M.

(Rus)

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

Comparison of mass properties of high- pressure cylinders with cryogenic fill for a throttle cooling system

Dovgjallo A.I., Sarmin D.V., Uglanov D.A.

(Rus)

Vol 19, No 1 (2020)

Method for optimizing mass and size characteristics of a high-pressure turbine disk

Siluyanova M.V., Grunin A.N., Alendar A.D., Kandaurov S.K.

(Rus)

Vol 15, No 4 (2016)

Increasing the efficiency of rotary piston engines by the use of the diesel cycle

Okorochkov V.V., Okorochkova V.M., Ravodin A.I.

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

Thermal state of a groind-use gas turbine engine stator

Grechishnikov O.V., Balakin A.Y., Roslyakov A.D.

(Rus)

Vol 18, No 4 (2019)

Formation of film cooling on the turbine blade back and pressure side in the case of using V-shaped dimples

Lebedev V.V., Lebedev O.V., Remizov A.E.

(Rus)

Vol 14, No 2 (2015)

Determination of thermal state and modification of the flame tube cooling system with the help of three-dimensional modeling methods

Matveev S.G., Anisimov V.M., Zubrilin I.A., Kolomzarov O.V., Mironov N.S.

(Rus)

Vol 11, No 3-2 (2012): Special Issue

Gas-turbine unit development experience for rotors wedging correction

Kozlyakova I.S., Krupin V.P., Potkin A.N., Fadeev V.A.

(Rus)

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

Motion trajectories of the vehicle with mass injection pre-compressor cooling turbojet engines as the first stage of aircraft-space systems

1 1., 1 1.

(Rus)

1 - 38 of 38 Items

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