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Title
Authors
Improving the efficiency of gas turbines by regenerating heat
Kulagin V.V., Sokolov M.A.
To the question of cooling power components of radio-electronic equipment by impinging freon jets
Lopatin A.A., Gortyshov Y.F.
Mixture modelling in a swirle flow in the ANSYS CFX program
Krasheninnikov S.V., Savchenko O.V.
System of pressurization of the fuel tank of a launch vehicle using the heat of generator gas
Biryuk V.V., Smorodin A.V., Shepelev A.I., Onoprienko D.A.
The effect of heat recovery on the optimal values of helicopter turboshaft engine parameters
Omar H.H., Kuz'michev V.S., Zagrebelnyi A.O., Grigoriev V.A.
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.
Development of an exhaust air turbine engine
Yeliseev Y.S., Fedorchenco D.G., Tsibizov Y.I., Tyulkin D.D., Tkachenko A.Y.
Experimental research of internal heat transfer in the vortex heat generator
Zhornik M.N., Piralishvili S.A., Mogileva K.A.
Peculiarities of heat transfer in thermoacoustic converters
Dovgyallo A.I., Nekrasova S.O.
Improving the efficiency of aviation turbofan engines by using an intercooler and a recuperative heat exchanger
Omar H., Kuz'michev V.S., Tkachenko A.Y.
New high-strength aluminum alloy on the basis of secondary materials
Barykin M.A., Naumova E.A., Belov N.A., Finogeev A.S., Koshmin A.N.
Inkjet heat transfer working model phone (fuel transportation) refrigerator drip emitters prospective spacecraft
1 1., 1 1., 1 1.
Features of calculation of hydraulic characteristics of capillary spray jets of is liquid-stnyh rocket engines of small pull-rod
1 1., 1 1., 1 1.
Thermophysical properties of multilayered structures
Rapilbekova N.S.
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.
Mathematical model of the “tank – nozzle” cooling system
Shalay V.V., Shcherban K.V.
Numerical simulation of heat transfer from a swirling flow to the lateral side of the vortex tube energy separation chamber
Piralishvili S.A., Sokolova A.A.
Obtaining the analytical solution of the heat boundary layer equation based on introducing additional boundary conditions
1 1., 1 1.
Influence of surface roughness on the heat transfer coefficient of fluids in an additively manufactured supercharger
Smekalkin A.S., Ivanov A.V.
Experimental testing of heat flux sensors based on the inverse problem technique
Alifanov O.M., Budnik S.A., Nenarokomov A.V., Titov D.M.
Heat engine cycle limitations imposed by fuel properties
Mikheyenkov E.L.
Development and analysis of models of heat transfer in compact porous heat exchangers of aero space control systems
Konovalov D.A.
Analysis of the thermal state of aircraft engine supports
Vinogradov A.S., Badykov R.R., Fedorchenko D.G.
Inkjet heat transfer working model phone (fuel transportation) refrigerator drip emitters prospective spacecraft
1 1., 1 1., 1 1.
Influence of pad geometry and method of oil supply on the thermal state of GTE rotor tilting-pad journal bearing
Parovay E.F.
Mathematical model for calculating the mass of a heat exchanger in problems of optimizing the parameters of the working process of aircraft gas turbine engines
Kuz'michev V.S., Omar H., Tkachenko A.Y., Bobrik A.A.
On the efficiency of a radiant heating regenerative system
Panchenko V.V.
Automated generation of structural members of a spacecraft thermal model
Kulikov D.S., Shatin A.A., Velmisov I.G.
Development of a methodology for calculating the working process of a small-size two-stroke internal combustion engine
Biryuk V.V., Gorshkalev A.A., Zakharov M.O., Larin V.L.
Increase of chrome-nickel steel 40ХН fatigue failure resistance by laser influence
Tregub V.I., Nikiforov A.M.
The experimental thermoacoustic device
Kharitonov A.A.
Morphological characteristics of the intermetallic phase of heat resisting nickel alloys
Kirikov S.V., Perevezentsev V.N., Tarasenko Y.P.
Heat meter for ASECM, integrated into TP management information system of an industrial enterprise
Biryuk V.V., Leonovich G.I., Livochkina N.A.
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.
Post-operation state and extension of service life of compressor blades of the gas-turbine power plant GTE-45-3
Tarasenko Y.P., Berdnik O.B., Tsareva I.N.
Adhesion strength of heat-insulating and wear-resistant ceramic coatings on aluminum alloys
Krishtal M.M., Ivashin P.V., Polunin A.V., Pavlov D.A., Nikerov K.N.
Forming of the structure and properties of titanium alloys according to mechanical properties in the processes of plastic working of metals
Tlustenko S.F., Pervyshin A.N.
Interaction of high-speed particles and temperature control elements of a space vehicle
Izyumov M.V., Syomkin N.D., Kalayev M.P.
Research of a seal work as an element of the air engine support
Vinogradov A.S., Rempel A.P.
Formation of microvortex gas flows in channels of a block catalyst with coplanar channels
Knysh Y.A., Tsibizov Y.I., Dmitriev D.N., Gorshkalev A.A.
Three-dimensional inhomogeneous thermal fields of the “Photon-Amur 2.0” payload electronic board developed for nanosatellites
Fomin D.V., Barulinа M.A., Golikov A.V., Strukov D.O., German A.S., Ogorodnikov A.A.
The determination of the thermoacoustic generator aspect from electrodynamic unit features by the parametric-studies
Vorotnikov G.V., Kruchkov A.N., Zynovyev E.A.
Investigation of thermal conditions of nanosatellite optoelectronic telescopic module for different modes of operation
Tsaplin S.V., Bolychev S.A.
Analysis of heat transfer in a helically coiled cooler of a mechatronic sample conditioning system
Gimadiev A.G., Utkin A.V.
Research of current and power interchange of swirled fluid streams in a hydraulic heat gentrator
Belozertsev V.N.
Efficiency of complex cycles of gas turbine units with air bleed for the cooling of intermediate combustion chambers
Ivanov V.A.
Regenerative air-water heat exchanger with improved heat exchange ability
Dostovalova S.S., Serebryakov R.A., Batukhtin S.G., Batukhtin A.G.
Heat exchange parameters of units and pipelines of the aircraft hydraulic system
Nikolayev V.N.
Structure and mehanpichesky properties of the shovel 1 steps of the rotor of turbine GTE-45-3 after the long operating time and regeneration
1 1., 1 1., 1 1.
Processing of experimental data by the method of the least squares
Ovchinnikov A.V., Krasnochub E.K., Bronstein V.M.
Mechanism of failure of working faces of big bearings in the process of operation
Melnikov A.A., Dmitrieva M.O.
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.
Analysis оf the cutting force of heat resisting alloys during high-speed milling
Khaimovich A.I., Kuznetsov A.V.
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.
Parametric analysis of thermoacoustic travelling-wave engine operation with external heat application
Dovgyallo A.I., Zynovyev Y.A., Vorotnikov G.V.
The simplification of heat engines thermodynamics calculation with using of idaeal gas’ model
1 1., 1 1.
Investigation of friction joints working in nuclear plant with heat transfer medium consist of heavy high temperature liquid metal
Drozdov Y.N., Beznosov A.V., Makarov V.V., Puchkov V.N., Antonenkov M.A., Kuznetsov D.V.
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.
Problems of heat and mass transfer on phase transformations or hemical reaction
Churkina N.V.
Analysis of control programs and climb paths of the hypersonic first stage of an aerospace system
Balakin V.L., Krikunov M.M.
Thermal design of «AIST» small spacecraft
Kulikov D.S., Erilkin J.N.
Experimental investigation of heat transfer in energy separation chambers of the vortex tube
Veretennikov S.V., Barinov S.N.
Experimental research of heat exchange in a plane channel using the regular thermal regime mrthod with different Biot numbers
Kolesova E.G., Veretennikov S.V., Zhornik M.N.
Development of a calculation method for control system of radial clearance in the turbine of gas turbine engine
Bondarchuk P.V., Tisarev A.Y., Lavrushin M.V.
Research of a heat-resistant intermetallic underlayer for the heat-shielding coating of gas turbine engine turbine blades
Tarasenko Y.P., Tsareva I.N., Berdnik O.B., Fel Y.A., Krivina L.A.
Methodology of analysis temperature stresses in chips
Krasnoschekova G.F., Tyulevin S.V., Nasedkin A.V., Mishanov R.O.
Processing of experimental data by the method of the least squares
1 1., 1 1., 1 1.
Modeling of heat conduction process in porous MR material
1 1.
Computer-aided-design system for calculating adsorption thermodynamic characteristics
Zelenko L.S., Varfolomeyeva V.V., Kuznetsov V.Y., Fed’kayev A.V., Terentyev A.V., Buryak A.K.
Mathematical modeling of the process of selective laser melting of Ti-6Al-4V titanium alloy powder
Agapovichev A.V., Sotov A.V., Smelov V.G.
Analisys of experimental combustion chambers fire tests for LRE with cooling by liquid oxigen for "DM" type booster
Smolentsev A.A., Strizhenko P.P.
Comparison of heat generation estimation methods for angular contact ball bearings
Petrov N.I., Lavrentyev Y.L.
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.
Strength analysis of internal combustion engine elements by using ANSYS with taking into account heat processes in the combustion chamber
Biryuk V.V., Gorshkalev A.A., Kayukov S.S., Saigakov E.A.
Automated thermovacuum firing test facility for testing and research of workflow in low-thrust rocket engine on hypergolic propellants
Galperin R.N., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.
Increase in thermal efficiency of the conditioned clothing
Savchenko N.V.
A hot-wire anemometric transducer of airflow mass rate
Nikolayev V.N.
Automated selection of cooling system for radio electronic design of thermophysical
Goryachev N.V., Trusov V.A., Yurkov N.K.
Energy sources in heat engine cycles
Mikheyenkov E.L.
Investigation of the thermal regime of microsatellite optoelectronic telescopic complex under operating conditions
Tsaplin S.V., Bolychev S.A.
The influence of residual technological stress and service heat loads on the strength of railway wheels
Kerentcev D.E., Ponomarev J.K.
The influence of the shuttle effect on the intensification of heat losses in a Stirling engine
Savchenko V.A., Stolyarov S.P.
The modeling of the thermoacoustic electric generator by quadrupole approximation approach
Vorotnikov G.V.
The solution of an uncoupled thermoelastic problem with a displacement vector and a heat flow defined on a body boundary
Makarova I.S.
Investigation of thermal conditions nozzle blades with a cyclone-vortex cooling system
Veretennikov S.V., Khasanov S.M.
Particularity of thermal condition computation oF LRE with cooling by liquid oxygen
1 1.
Development of a generalized model of heat-mass transfer between fuel drops and gas stream with reference to gas turbine engine combustion chambers
Tretyakov V.V., Sviridenkov A.A.
Analysis of the properties of water condensate obtained from heat engine exhaust yases
Knysh Y.A., Uglanov D.A.
Common properties of hydrocarbon combustion products and Brayton cycle
Mikheenkov E.L.
The calculation of optimum worker frequencies of the thermoacoustic electric generator with including ready electrodynamic unit and given load
Vorotnikov G.V., Kryuchkov A.N.
Using heat pipes to improve the efficiency of gas-dynamic thermal stratification
Tsynaeva A.A., Tsynaeva E.A., Shkolin E.V.
Vortex effect and intensification of heat and mass transfer in cell energy technology
Piralishvily S.A., Veretennikov S.V.
Influence of the loading parameter on the efficiency ofa three-stage turbine of turbojet bypass engine
1 1., 1 1.
Applying the possibilities of Microsoft Excel for solving problems of fuel burning thermodynamics
Mikheenkov E.L., Nekrasova S.O., Ramzaeva E.A.
Modeling of heat conduction process in porous MR material
Zhizhkin A.M.
Using an ionization probe removed from the sparking plug for the development of a two-zone ICE combustion model
Ivashin P.V., Rybakov M.P.
Vortex cleaning of fuel tank pressurant gas
Biryuk V.V., Shimanov A.A., Onoprienko D.A., Smorodin A.V., Shepelev A.I.
Mathematic simulation of AL-31F powerplant radiation in the IR range
Filippov G.S.
Formation in the channels of the block catalyst the micro vortex gas flows with intense twist
Knysh Y.A., Zibizov Y.I., Dmitriev D.N., Gorshkalev A.A.
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.
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