Experimental research of the possibility of heat transfer enhancement in gas dynamic energy separation process
Popovich S.S., Vinogradov Y.A., Strongin M.M.
Automated generation of structural members of a spacecraft thermal model
Kulikov D.S., Shatin A.A., Velmisov I.G.
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.
Methodology of analysis temperature stresses in chips
Krasnoschekova G.F., Tyulevin S.V., Nasedkin A.V., Mishanov R.O.
Theoretical and experimental analysis of the thermal state of transport aircraft compartments thermal state
Nikolayev V.N.
Analysis of the thermal state of aircraft engine supports
Vinogradov A.S., Badykov R.R., Fedorchenko D.G.
Numerical simulation of the working process in a vortex tube with an additional stream
Vasilyuk O.V., Piralishvili S.A., Shaykina A.A.
Modeling thermal and thermomechanical effects in elements of microcircuits for the design of aircraft control airborne equipment
Fortinsky Y.K.
Limit values of the Brayton cycle with the use of reduced fuel characteristics
Mikheenkov E.L., Nekrasova S.O.
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.
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.
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.
Thermodynamic calculation of a thermomechanical compressor
Blagin E.V., Dovgyallo A.I., Uglanov D.A., Dostovalova S.S.
Optimal design of an induction heater of minimum length
Mednikova V.A.
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.
Applying the possibilities of Microsoft Excel for solving problems of fuel burning thermodynamics
Mikheenkov E.L., Nekrasova S.O., Ramzaeva E.A.
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.
Vacuum capacitors with high temperature stability
Ryzhov A.A., Jurkov N.K., Romashin A.A.
Experience of operational development of starting characteristics of the APU combustion chamber
Chechulin A.Y.
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.
Transducer of fluid and air consumption and temperature in pipelines
Nikolayev V.N., Kabanov Y.N.
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.
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.
Dependence of energy characteristics of Stirling gas refrigerating machines on external and internal parametric values
Belozertsev V.N.
The analysis of real thermodynamic cycle of bypass engine with mixing
Medvedev V.V.
Thermophysical properties of multilayered structures
Rapilbekova N.S.
Results of hot tests of an oxygen preburner of a liquid-propellant engine 11D58MF
Barsukov O.A., Strizhenko P.P.
Use of control volume method for the temperature field calculation by laser influence
Murzin S.P., Mezhenin A.V., Osetrov E.L.
Experimental research of wall boundary flow formation in the combustion chamber of a small gas generator with self-igniting fuel components
Shustov S.A.
Criterial approach to constructing empirical models of cutting
Vinokurov M.V., Druzhin A.N.
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.
Calculation of cutting temperature at milling of purveyances from hard-processing materials
Trusov V.N., Skuratov D.L., Zakonov O.I., Shikin V.V.
Development of the active gas generator for high altitude firing test benches
Salich V.L.
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.
Theoretical definition of temperature fields at thermoplastic hardening of details of gas turbine engines
Barvinok V.A., Vishnyakov M.A., Ignatiev S.A.
Parameters study in the electrothermal and jet protection of the airliner cockpit windows from fogging
Nikolayev V.N.
Centrifugal force field effect consideration in dynamics investigation of blade wheels
Davydov D.P., Ermakov A.I.
Relation between flame chemiionization and variable-volume combustion chamber temperature and pressure
Shaikin A.P., Galiev I.R.
Thermal deformation influence to cryogenic pumps seals operability
Ivanov A.V.
Increase in thermal efficiency of the conditioned clothing
Savchenko N.V.
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.
To the question of cooling power components of radio-electronic equipment by impinging freon jets
Lopatin A.A., Gortyshov Y.F.
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.
The community of the ideal and complex cycles of the gas-turbine installations
Ivanov V.A.
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.
Obtaining the analytical solution of the heat boundary layer equation based on introducing additional boundary conditions
1 1., 1 1.
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.
Peculiarities of gas temperature field formation at the exit of small-sized gas turbine engine combustion chambers
1 1., 1 1., 1 1.
The equipment for research of properties of hydrocarbons at pressure from above 150 MPа
Rednikov S.N.
The machine and methods of tribotehnical tests of materials
Ibatullin I.D., Zhuravlev A.N., Utjankin A.V., Galljamov A.R., Neyaglova R.R.
Investigation of thermal conditions of nanosatellite optoelectronic telescopic module for different modes of operation
Tsaplin S.V., Bolychev S.A.
Design solutions to provide thermal protection of three-shaft turbofan engine turbine support oil cavities
Petrukhin A.G., Boev A.A., Butylkin S.V.
Interaction of high-speed particles and temperature control elements of a space vehicle
Izyumov M.V., Syomkin N.D., Kalayev M.P.
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.
Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines
Ryzhkov V.V., Morozov I.I.
Dependence of required turbine inlet temperature at cruise mode of long-term flight on bypass ratio
Rybakov V.N.
Research of current and power interchange of swirled fluid streams in a hydraulic heat gentrator
Belozertsev V.N.
Investigation of the thermal regime of microsatellite optoelectronic telescopic complex under operating conditions
Tsaplin S.V., Bolychev S.A.
On the efficiency of a radiant heating regenerative system
Panchenko V.V.
Harmonic model of thermodynamic cycle in thermoacoustic engine regenerator
Zynovyev E.A., Dovgyallo A.I., Vorotnikov G.V.
To a question of forcing up of thermal stirlings macine
Belozertcev V.N.
Thermal control of spacecraft star sensor attitude control system based on the solution of a coupled thermoelasticity problem
Tsaplin S.V., Bolychev S.A.
Surging and auto-off the helicopter engine at start-up unguided missile from launchers
Prokopiev A.L., Povetkin O.V.
Ground testingresults of loop heat pipe used to maintain thermal conditions of equipment
Biryuk V.V., Kitaev A.I.
Thermal design of «AIST» small spacecraft
Kulikov D.S., Erilkin J.N.
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.
Analysis of temperature fields of aircraft components
Azarenkov V.I.
Forecasting of the properties of structural materials and the choice of optimal technologies of their production
1 1., 1 1., 1 1., 1 1.
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.
Simulation and experimental development of a temperature control system of a radiation calibration source based on a PID-regulyator
Volkov V.V.
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