Pesquisa

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Modeling of convective heat transfer processes between inhomogeneous gas mixtures and surfaces of a small-caliber artillery barrel
Podkopaev I., Podkopaev A., Dolzhikov V.
Conversion use of models of working processes of rocket engine turbine installations in the application to local power engineering
Abroskin V., Chernorot V., Kishkin A., Delkov A., Zhuravlev V.
To the task of controlling a group of objects on the basis of information technologies
Zhalnin D.
Design of a thermal control system with a two-phase coolant for a spacecraft with a capacity of 7 kW
Shilkin O., Kolesnikov A., Delkov A., Kishkin A., Shevchenko Y.
Development of a mobile device for collection of heat power parameters of the refrigerator
Shurinova D., Suvorov A., Kovalenko A., Murygin A.
Solar thermal propulsion systems with various high-temperature power sources
Finogenov S., Kolomentsev A.
Simulation of the induction soldering process of waveguide paths from aluminum alloys
Bocharova O., Murygin A., Bocharov A., Zaitsev R.
Development of the heat panel of the small space apparatus for navigation support
Kolga V., Yarkov I., Yarkova E.
Heat transfer in the centrifugal force field for gas turbines elements
Zuev A., Arngold A., Khodenkova E.
Determining thermal resistance in the model of the liquid circuit of spacecraft thermal control system
Shevchenko Y., Kishkin A., Tanasienko F., Shilkin O., Popugayev M.
Local heat transfer parameters in the areas of the developing temperature boundary layer in the cavities of gas turbines local heat transfer parameters in the areas of the developing temperature boundary layer in the cavities of gas turbines
Zuev A., Arngol'd A., Falkova E., Tolstopyatov M., Dubynin P.
The choice of the energy parameters of an oxygen-hydrogen propellant expander cycle rocket engine
Belyakov V.
Identification and simulation mathematical model of thermo and physical loading of a small-caliber artillery barrel
Podkopaev A., Babadzanov A., Podkopaev I., Dolzhikov V.
Increasing the specific impulse of an oxygen-hydrogen liquid rocket engine by increasing heat transfer in the combustion chamber
Vasilevsky D.
To the task of controlling a group of objects on the basis of information technologies
Zhalnin D.
Calculation of complex heat transfer in the liquid circuit of the spacecraft thermal control system based on real topology and thermophysical properties
Shevchenko Y., Kishkin A., Tanasienko F., Shilkin O., Sokolov S.
Design of the cooling system of a reasuble liquid rocket engine with three-component fuel
Belyakov V., Vasilevsky D., Ermashkevich A., Kolomentsev A., Farizanov I.
THE STUDY OF THE FLOW IN THE VAPOUR CHANNEL OF SHORT LINEAR HEAT PIPES
Seryakov A.
ROTATIONAL FLOWS HEAT TRANSFER IN TURBOMACHINES BASED ON TWO-LAYER MODEL OF TURBULENT BOUNDARY LAYER
Zuev A., Kishkin A., Tolstopyatov M., Zhuykov D.
INSTALLATION FOR EXPERIMENTAL RESEARCH OF CONVECTIVE HEAT OF THE ROTATIONAL GAS FLOW
Zuev A., Tolstopyatov M., Zhuikov D.
COMPUTATIONAL EXPERIMENT ON OBTAINING THE CHARACTERISTICS OF A THERMAL CONTROL SYSTEM OF SPACECRAFT
Tanasienko F., Shevchenko Y., Delkov A., Kishkin A., Melkozerov M.
MODELING OF PROCESSES OF HEAT AND MASS TRANSFER IN MICROCHANNEL HEAT EXCHANGERS OF SPACE-SYSTEM ENGINEERING CONTROL SYSTEMS
Konovalov D., Kozhukhov N., Drozdov I.
BUNDLED SOFTWARE TO COMPUTE TEMPERATURE FIELDS OF SPACE VEHICLES PANELS WITH LEAKY CONSTRUCTION
Vasiljev E., Derevyanko V.
MATHEMATICAL MODEL OF HEAT EXCHANGE PROCESSES IN HONEYCOMB PANELS WITH HEAT PIPES
Vasilyev E., Derevyanko V.
The research of effective thermal conductivity coefficient effect on the temperature field of reflector
Burova O., Romankov E., Tsivilev I., Minakov A.
RESULTS AND PROSPECTS OF JOINT HEAT PHYSICAL RESEARCHES OF ICM OF THE SB RAS AND JSC “ACADEMICIAN M.F. RESHETNEV “INFORMATION SATELLITE SYSTEMS”
Shaidurov V., Derevyanko V., Vasilyev E., Kosenko V., Zvonar V., Chebotarev V.
THERMAL PROPERTIES, MAGNETOAND BAROCALORIC EFFECTS IN La0.7Pb0.3MnO3 SINGLE CRYSTAL
Kartashev A., Bogdanov E., Pogoreltsev E., Gerasimova Y.
Thermo anemometric transducer of airflow mass velocity
Nikolaev V., Nikolaev V.
SYNTHESIS, STRUCTURE, EPR SPECTRA AND HEAT CAPACITY OF CUBIC CsZnMoO 3F 3 OXYFLUORIDE
Molokeev M., Petrakovskaya E., Bondarev V., Kolesnikova E., Ivanov N.
THE ANALYSIS OF THERMOELECTRIC MODULE EFFICIENCY IN THE COOLING SYSTEMS
Vasilyev E., Derevyanko V.
NUMERICAL AND STATISTICAL METHOD FOR SOLVING THE HEAT EXCHANGE PROBLEMS IN THE HEAT-PROTECTIVE CONSTRUCTIONS OF THE HONEYCOMB TYPE
Gusev S., Nikolaev V.
APPLICATION OF STEAM JET NOZZLE IN HEAT PIPES OF MEAN TEMPERATURE RANGE
Seryakov A., Konkin A., Belousov V.
THE ORGANIZATION OFTHE LIGHT PRESSUREON THE SATELLITE SURFACEACCOUT
Shilko I., Shilko I.
NUMERICAL RESEARCH OF STATIONARY MODES IN TECHNOLOGICAL FURNACES
Demidenko N., Alsov M.
Calculation of eigenvalues in the problem of unsteady heat transfer through a cylindrical wall with mixed boundary conditions
Vidin Y., Ivanov D.
SOLAR THERMAL PROPULSION WITH DIFFERENT TYPES OF CONCENTRATOR-ABSORBER SYSTEM
Finogenov S., Kolomentsev A., Nazarov V.
DISTRIBUTED PARAMETERS ENERGY-HEAT MODEL OF SPACE NICKEL-HYDROGEN STORAGE BATTERY
Sakhnov M., Lelekov A., Galochkin S., Sahnov M., Lelekov A., Galochkin S.
HEAT TRANSFER IN THE CAVITY OF A GAS TURBINE LIQUID ROCKET ENGINE
Zuev A., Tolstopyatov M.
TWO-DIMENSIONAL THERMAL MODEL OF THE THERMAL CONTROL SYSTEM FOR NONHERMETIC FORMATION SPACECRAFT
Tanasienko F., Shevchenko Y., Delkov A., Kishkin A.
THE MEASUREMENT OF THE CONDENSATE FILM THICKNESS OF THE WORKING FLUID BY MEANS OF THE CAPACITIVE SENSORS IN THE LOW-TEMPERATURE RANGE HEAT PIPES
Seryakov А., Mikhailov Y., Shakshin S.
APPLICATION OFTHE COMBINED HEATING SYSTEMS IN ELECTRIC HOLDINGFURNACES FOR PREPARATION OFALUMINIUMALLOYS
Temerov A., Timofeev V., Mikhaylov D., Temerov A., Timofeev V., Mikhaylov D.
DEVELOPMENT AND THERMAL VACUUM TESTS OF HEAT SHIELDS FOR PROTECTION OF MECHANICAL ELECTRIC DRIVE UNIT FROM EFFECT OF “SOLAR TRAP”
Vshivkov A., Tanasienko F., Golovenkin E., Yurtaev E.
STEAM TURBINES WITH LOW-BOILING WORKING MEDIUM
Morozov N., Karasev V., Morozov N., Karasev V.
ENERGY-TECHNOLOGYCONVERSION OFBROWN COALOF BALAKHTACOALDEPOSIT: INNOVATIVEAPPROACH TO ENERGYEFFICIENCY IN THE REGION
Mikhalev I., Islamov S., Mikhalev I., Islamov S.
DEVELOPMENT OF THE METHODOLOGY OF ELECTRIC THERMAL VACUUM TESTING FOR TEMPERATURE CONTROL OF SMALL SPACECRAFT JUBELEE-2 (MIR)
Vshivkov A., Golovenkin E., Krat S., Ganenko S.
MODELING OF THERMAL OBJECTS WITH DISTRIBUTED PARAMETERS WITH THE USE OF COMSOL MULTIPHYSICS-MATLAB-SIMULINKSOFTWARE PACKAGES
Lelekov A., Sakhnov M., Galochkin S., Velichko E., Lelekov A., Sahnov M., Galochkin S., Velichko E.
Heat capacity, thermal expansion and caloric effects in ferroelectric-ferromagnetic composite 0.82(PbTi 0.3) - 0.18(La 0.7Pb 0.3Mn0 3)
Mikhaleva E., Mikhashenok N., Molokeev M., Flerov I., Gorev M.
MODELING OF SPECTROERERGETIC CHARACTERISTICS OF SPACE OBJECTS IN THE OPTICAL RANGE
Bogoyavlenskiy A., Kamenev A., Poluyan M., Soluyanov A.
Rectilinear uniform gas flow with thermal efficiency in propulsion equipment of aircrafts
Tolstopyatov M., Zuev A., Kishkin A., Zhuikov D., Nazarov V.
MATHEMATICAL MODEL OF HEAT EXCHANGE PROCESSESIN THE HONEYCOMB PANEL WITH HEAT PIPES
Vasil'ev E., Derevyanko V., Vasilyev E., Derevyanko V.
INVESTIGATION OF TWO PHASE LOOP THERMAL CONTROL SYSTEM WITH DEPLOYABLE RADIATOR OF TELECOMMUNICATION SATELLITE WITH HIGH LEVEL OF HEAT OUTPUT
Krivov E.
CALCULATION OF CHARACTERISTICS OF THERMOELECTRIC COOLING SYSTEM OF HEAT-LOADED ELEMENTS OF RADIO ELECTRONIC EQUIPMENT
Vasil’ev E.
HEAT TREATMENT EFFECT ON THE SEPARATE PHASES DEFORMATIONS IN ALLOYALMG10 AND ALCU4MG1.5
Grechnikov F., Nosova E., Savelyeva O.
STEAM TURBINES WITH A LOW-BOILING WORKING AGENT
Morozov N., Karasev V.
FLAT HEAT PIPES FOR HEAT REMOVAL FROM ELECTRONIC EQUIPMENT IN SPACE VEHICLES
Derevyanko V., Nesterov D., Kosenko V., Zvonar V., Chebotarev V., Fatkulin R., Suntsov S.
NUMERICAL SIMULATION OF MODIFYING MATERIAL DISTRIBUTION DURING THE IMPULSE INDUCTION HEATING OF METAL SURFACE
Popov V.
1 - 56 de 56 resultados
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