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Automated generation of structural members of a spacecraft thermal model

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

(Rus)

Vol 10, No 6 (2011)

Transducer of fluid and air consumption and temperature in pipelines

Nikolayev V.N., Kabanov Y.N.

(Rus)

Quasi one-dimensional model and calculation of processes in gas turbineengine combustion chambers given the heterogeneity of the combustible mixture, changes in mass, composition, temperature and stirring efficiency of the working body

Didenko A.A., Sokolov A.B.

(Rus)

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

Surging and auto-off the helicopter engine at start-up unguided missile from launchers

Prokopiev A.L., Povetkin O.V.

(Rus)

Vol 16, No 1 (2017)

On the efficiency of a radiant heating regenerative system

Panchenko V.V.

(Rus)

Vol 10, No 5 (2011)

Research of current and power interchange of swirled fluid streams in a hydraulic heat gentrator

Belozertsev V.N.

(Rus)

Vol 11, No 7 (2012)

Vacuum capacitors with high temperature stability

Ryzhov A.A., Jurkov N.K., Romashin A.A.

(Rus)

Design solutions to provide thermal protection of three-shaft turbofan engine turbine support oil cavities

Petrukhin A.G., Boev A.A., Butylkin S.V.

(Rus)

Vol 13, No 2 (2014)

Methodology of analysis temperature stresses in chips

Krasnoschekova G.F., Tyulevin S.V., Nasedkin A.V., Mishanov R.O.

(Rus)

Vol 8, No 4 (2009)

Interaction of high-speed particles and temperature control elements of a space vehicle

Izyumov M.V., Syomkin N.D., Kalayev M.P.

(Rus)

Vol 7, No 3 (2008): Special Issue

Ground testingresults of loop heat pipe used to maintain thermal conditions of equipment

Biryuk V.V., Kitaev A.I.

(Rus)

Mathematical model for calculating radial non-uniformity of the gas temperature field at the exit of small gas turbine engine combustion chambers

Lukachev S.V., Abrashkin V.Y., Lansky A.M., Matveev S.G.

(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 15, No 3 (2016)

Influence of the burner form on the combustion chamber outlet temperature field ripple for different modes of operation of gas turbine engines

Markushin A.N., Baklanov A.V.

(Rus)

Vol 14, No 2 (2015)

Experience of operational development of starting characteristics of the APU combustion chamber

Chechulin A.Y.

(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 11, No 2 (2012)

Numerical simulation of gas temperature spatial distribution in a full-size gas turbine combustor and its one-burner sector

Kostyuk V.Y., Kirilash Y.I., Stasyuk A.V., Shein V.V., Karzov D.V.

(Rus)

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

The machine and methods of tribotehnical tests of materials

Ibatullin I.D., Zhuravlev A.N., Utjankin A.V., Galljamov A.R., Neyaglova R.R.

(Rus)

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

Forecasting of the properties of structural materials and the choice of optimal technologies of their production

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

(Rus)

Vol 7, No 2 (2008)

Use of control volume method for the temperature field calculation by laser influence

Murzin S.P., Mezhenin A.V., Osetrov E.L.

(Rus)

Conditions of compatibility of compressor and turbine used as part of a gas generator required to ensure turbine operability

Grigoriev A.V., Ilyushin M.Y., Mitrofanov V.A., Rassokhin V.A., Rudakov O.A., Solovieva A.V.

(Rus)

Vol 18, No 2 (2019)

Investigation of thermal conditions of nanosatellite optoelectronic telescopic module for different modes of operation

Tsaplin S.V., Bolychev S.A.

(Rus)

Vol 15, No 2 (2016)

Thermal control of spacecraft star sensor attitude control system based on the solution of a coupled thermoelasticity problem

Tsaplin S.V., Bolychev S.A.

(Rus)

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

Research of influence of the thermal stream from the mid-flight liquid rocket engine on parameters of operating liquid rocket engines of small draught in the conditions of perspective razgonnogo's propulsion system of the block

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

(Rus)

Vol 11, No 2 (2012)

Numerical simulation of gas temperature spatial distribution in a one-burner sector of a gas turbine combustor with uncertain initial conditions of fuel atomization

Kostyuk V.Y., Kirilash Y.I., Stasyuk A.V., Shein V.V., Karzov D.V.

(Rus)

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

Calculation of cutting temperature at milling of purveyances from hard-processing materials

Trusov V.N., Skuratov D.L., Zakonov O.I., Shikin V.V.

(Rus)

Theoretical definition of temperature fields at thermoplastic hardening of details of gas turbine engines

Barvinok V.A., Vishnyakov M.A., Ignatiev S.A.

(Rus)

Vol 7, No 1 (2008)

Experimental investigations of thermal fields in inductor system under magnetic pulse forming

Barvinok V.A., Palamartchuk Y.Y., Kirilin A.N., Samokhvalov V.P., Vershigorov V.M.

(Rus)

Method of reduced fuel characteristics and parameters of the operating cycles of heat engines

Anastaseev V.V., Belozertsev S.V., Mikheenkov E.L., Nekrasova S.O.

(Rus)

Vol 18, No 1 (2019)

Development of the active gas generator for high altitude firing test benches

Salich V.L.

(Rus)

Vol 15, No 1 (2016)

Thermal design of «AIST» small spacecraft

Kulikov D.S., Erilkin J.N.

(Rus)

Vol 14, No 1 (2015)

Electrization of the surface of low-orbiting small spacecraft “AIST”

Syomkin N.D., Bragin V.V., Piyakov A.V., Telegin A.M., Ryazanov D.M., Matviets M.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 5-1 (2012): Special Issue

Dependence of required turbine inlet temperature at cruise mode of long-term flight on bypass ratio

Rybakov V.N.

(Rus)

Vol 10, No 1 (2011)

Modeling thermal and thermomechanical effects in elements of microcircuits for the design of aircraft control airborne equipment

Fortinsky Y.K.

(Rus)

Centrifugal force field effect consideration in dynamics investigation of blade wheels

Davydov D.P., Ermakov A.I.

(Rus)

Vol 12, No 2 (2013)

Thermophysical properties of multilayered structures

Rapilbekova N.S.

(Rus)

Vol 20, No 4 (2021)

Choice of gas temperature at the turbopump turbine inlet

Ivanov A.V.

(Rus)

Vol 17, No 3 (2018)

Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines

Ryzhkov V.V., Morozov I.I.

(Rus)

Vol 14, No 4 (2015)

Analysis of temperature fields of aircraft components

Azarenkov V.I.

(Rus)

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

Dependence of energy characteristics of Stirling gas refrigerating machines on external and internal parametric values

Belozertsev V.N.

(Rus)

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

Lopatin A.A., Gortyshov Y.F.

(Rus)

Vol 10, No 1 (2011)

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

Nikolayev V.N.

(Rus)

Thermal deformation influence to cryogenic pumps seals operability

Ivanov A.V.

(Rus)

Vol 12, No 2 (2013)

Optimal design of an induction heater of minimum length

Mednikova V.A.

(Rus)

Vol 16, No 4 (2017)

Simulation and experimental development of a temperature control system of a radiation calibration source based on a PID-regulyator

Volkov V.V.

(Rus)

Vol 14, No 3-2 (2015): Special Issue

Influence of tool deterioration on the density of heat flux distribution in the cutting area in end milling of OT4 titanium alloy

Evdokimov D.V., Skuratov D.L.

(Rus)

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

Influence of argon, propane and ethane viscous dissipation on the thermal state of a porous plate

Baygaliev B.E., Tumakov A.G., Tumakov E.A., Ibragimov A.I.

(Rus)

The analysis of real thermodynamic cycle of bypass engine with mixing

Medvedev V.V.

(Rus)

Vol 9, No 1 (2010)

Obtaining the analytical solution of the heat boundary layer equation based on introducing additional boundary conditions

1 1., 1 1.

(Rus)

Wearability, wearproof and heat-shielding coverings for details of the gas path of the turbine, the compressor and the chamber of combustion of gas turbine engine

Barvinok V.A., Shitarev I.L., Bogdanovich V.I., Dokukina I.A., Karasev V.M.

(Rus)

Vol 12, No 2 (2013)

Experimental research of wall boundary flow formation in the combustion chamber of a small gas generator with self-igniting fuel components

Shustov S.A.

(Rus)

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

Harmonic model of thermodynamic cycle in thermoacoustic engine regenerator

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

(Rus)

Vol 16, No 4 (2017)

Relation between flame chemiionization and variable-volume combustion chamber temperature and pressure

Shaikin A.P., Galiev I.R.

(Rus)

Vol 14, No 3-2 (2015): Special Issue

Formation of a model of rheological properties of hard-to-machine materials in the process of intensive cutting force deflection

Khaimovich A.I., Balaykin A.V., Galkina N.V.

(Rus)

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

Results of hot tests of an oxygen preburner of a liquid-propellant engine 11D58MF

Barsukov O.A., Strizhenko P.P.

(Rus)

Research of influence the processes to afterhardening glass transition temperature of PKM

Postnov V.I., Burhan O.L., Rahmatullin A.E., Mantusova O.Y., Nikitin E.K.

(Rus)

Numerical simulation of the working process in a vortex tube with an additional stream

Vasilyuk O.V., Piralishvili S.A., Shaykina A.A.

(Rus)

Vol 9, No 1 (2010)

Peculiarities of gas temperature field formation at the exit of small-sized gas turbine engine combustion chambers

1 1., 1 1., 1 1.

(Rus)

Vol 8, No 2 (2009)

Developing an electronic reference book on thermogasodynamic properties of rocket engine fuel combustion products taking into account non-ideal character of the working process

Silyutin M.V.

(Rus)

Applying the possibilities of Microsoft Excel for solving problems of fuel burning thermodynamics

Mikheenkov E.L., Nekrasova S.O., Ramzaeva E.A.

(Rus)

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

To a question of forcing up of thermal stirlings macine

Belozertcev V.N.

(Rus)

Vol 16, No 2 (2017)

Investigation of the thermal regime of microsatellite optoelectronic telescopic complex under operating conditions

Tsaplin S.V., Bolychev S.A.

(Rus)

Vol 10, No 5 (2011)

The concept of matching the joint operation of the combustion chamber, the compressor and the turbine

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

The equipment for research of properties of hydrocarbons at pressure from above 150 MPа

Rednikov S.N.

(Rus)

Thermodynamic calculation of a thermomechanical compressor

Blagin E.V., Dovgyallo A.I., Uglanov D.A., Dostovalova S.S.

(Rus)

Vol 8, No 4 (2009)

Criterial approach to constructing empirical models of cutting

Vinokurov M.V., Druzhin A.N.

(Rus)

Vol 7, No 3 (2008): Special Issue

The community of the ideal and complex cycles of the gas-turbine installations

Ivanov V.A.

(Rus)