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Mathematical modeling of autocompensation devices
Katkova V.P., Vyakhirev V.A., Krintal A.N.
Mathematical model of a linear electrodynamic engine operation on impact with account for elastic deformation of the hardened surface
Shvaleva N.A., Fadeev A.A., Eresko T.T.
Mathematical model of reliability of information processing computer appliances for real-time control systems
Aab A.V., Galushin P.V., Popova A.V., Terskov V.A.
Mathematical model of the mirror system of the Millimetron observatory and a description of the method of pre-measurement of the telescope within this model
Makarov S.N., Verhoglyad A.G., Stupak M.F., Ovchinnikov D.A., Oberemok Y.A.
Method for calculating the optimal geometry of a vortex ejector
Kuznetsov V.I., Makarov V.V., Shchuka I.O.
Mathematical model of a linear electrodynamic engine operation on impact with account for elastic deformation of the hardened surface
Shvaleva N.A., Fadeev A.A., Eresko T.T.
Design of the cooling system of a reasuble liquid rocket engine with three-component fuel
Belyakov V.A., Vasilevsky D.O., Ermashkevich A.A., Kolomentsev A.I., Farizanov I.R.
Development of the concept of a reusable liquid rocket engine with three-component fuel
Belyakov V.A., Vasilevsky D.O., Ermashkevich A.A., Kolomentsev A.I., Farizanov I.R.
Increasing the specific impulse of an oxygen-hydrogen liquid rocket engine by increasing heat transfer in the combustion chamber
Vasilevsky D.O.
Optimal control of deployment of the spoke of a transformable reflector in the presence of disturbances
Kabanov S.A., Kabanov D.S., Nikulin E.N., Mitin F.V.
Optimal control of deployment of the spoke of a transformablereflector in the pres-ence of disturbances
Kabanov S.A., Kabanov D.S., Nikulin E.N., Mitin F.V.
Solution of the filtration problem with the optimal adjustment of the radio-reflecting net of a transformable reflector
Kabanov S.A., Mitin F.V.
The aircraft hydraulic system units and pipelines heat exchange parameters study
Nikolaev V.N.
RELIABILITYGROWTHAND ENERGETIC EFFICIENCYOF ELECTRIC HEATINGSYSTEMS OF ELECTRIC HOLDING FURNACES FORALUMINIUMALLOYS
Temerov A.A., Timofeev V.N., Mikhaylov D.A., Temerov A.A., Timofeev V.N., Mikhaylov D.A.
CALCULATION OF UNCLOSED AXIAL HYDROSTATIC BEARING CHARACTERISTICS WITH ACCOUNT OF BEARING SURFACE AREA ROUGHNESS
Strok L.V., Sekatskiy V.S., Pikalov Y.Y., Brungardt M.V.
Numerical simulation of electron-beam welding with a longitudinal oscillation of the beam based on the experimental determination of the keyhole form
Permyakov G.L., Trushnikov D.N., Belenkiy V.Y., Olshanskaya T.V.
PARAMETRIC IDENTIFICATION OF THE HEAT CONDITION OF RADIO ELECTRONIC EQUIPMENTIN AIRPLANE COMPARTMENT
Gusev S.A., Nikolaev V.N.
Thermo anemometric transducer of airflow mass velocity
Nikolaev V.N., Nikolaev V.N.
Comparison of direct and reverse cycle of the thermal control system for the non-hermetic spacecrafts
Delkov A.V., Hodenkov A.A., Shevchenko Y.N.
MATHEMATICAL MODEL OF OIL PRICE FORMING ADJUSTED FOR TIGHT OIL FACTOR
Safonov K.V., Yushkov A.S., Lytkina L.I.
Method of optimum control of electrolyte chemical composition at aluminum production
Piskazhova T.V.
THE PROBLEM OF CONSTRUCTION OF MATHEMATICAL MODELS FOR OPTIMIZATION OF PARAMETERS OF FRICTION DAMPERS ON THE EXAMPLE OF BLADES OF GAS TURBINE ENGINES
Rеpetskiy O.V., Phan V.T.
Results of computing experiments at mathematical modeling of water ecosystems
Petrov Y.S., Raspopov V.E.
APPLICATION OF GENETIC ALGORITHMS TO COPE WITH A TASK OF ESTIMATION OF REGIONAL INDUSTRIAL POLITICS EFFECTIVE STRENGT
Gorbunov М.А., Medvedev А.V., Semenkin Е.S.
PROGRAM COMPLEX FOR MODELING OF STABILIZED MOTION OF SPACECRAFT WITH TRANSFORMABLE FLEXIBLE PARTS
Ignatyev M.G., Kopylov V.M., Kulakov A.J., Sotnikov M.V.
Mathematical model of the ecranoplan parameters choice at the stage of the technical offer
Antipin M.L., Gusev I.N.
ABOUT LEGITIMACY OF USAGE OF AGREED PROBABILITIESOF FAILURE-FREE WORK AND AGREED BREAKDOWNS PROBABILITIESDENSITIES IN AGGREGATES RELIABILITY MATHEMATICAL MODELS
Boyko O.G., Boyko O.G.
DESIGN OPTIMIZATION OF THERMO-TECHNICAL SYSTEMS OPERATING IN A CLOSED CIRCUIT
Kishkin A.A., Delkov A.V., Khodenkov A.A., Zuev A.A., Zhuykov D.A.
“VIRTUAL CC&RP” - A MATHEMATICAL MODEL FOR THE CONTROL OF THE UNIT CC&RP AND ITS VISUALIZATION WITH THE HELP OF SOFTWARE PRODUCTS WinCC 7.0 AND Step 7
Piskazhova T.V., Sidelnikov S.B., Belolipetskii V.M., Yakivyuk P.N., Sidelnikov A.S.
EVALUATION OF THE DISTURBING MOMENT IN THE ANTENNA POINTING SYSTEM MOVEMENT SIMULATION
Goncharuk A.V., Lukyanenko M.V., Raevskiy V.A.
TECHNIQUE FOR CALCULATION AND SELECTION OF SPACECRAFT ELECTRIC HEATERS PARAMETERS UNDER UNCERTAINTY CONDITIONS
Chebotarev V.E., Zvonar V.D., Fatkulin R.F., Dmitriev G.B.
A MATHEMATICAL MODEL OF OIL PRICE ASSESSMENT
Safonov K.V.
MATHEMATICAL SIMULATION OF ELECTROPHORESIS OF LIVE CELLS BY MULTIELECTRODE DEVICE
Denisenko V.V., Zamay S.S., Zamay A.S.
APPLICATION OFTHE COMBINED HEATING SYSTEMS IN ELECTRIC HOLDINGFURNACES FOR PREPARATION OFALUMINIUMALLOYS
Temerov A.A., Timofeev V.N., Mikhaylov D.A., Temerov A.A., Timofeev V.N., Mikhaylov D.A.
THEORETICAL JUSTIFICATION OF ALGORITHM OF DETERMINATION OF AIRCRAFT ROTATING MASS MOMENTS
Ushakov N.U.
PRACTICAL POTENTIAL OF TECHNICAL COMPATIBILITY THEORY AT SPACE ENGINEERING AND RESCUE EQUIPMENT
Dvirniy V.V., Elfimova M.V., Dvirniy G.V., Patskova E.G.
METHOD FOR CALCULATING THE ENERGY CHARACTERISTICS AND SOLAR BATTERY PARAMETERS OF HIGH-VOLTAGE POWER SUPPLY SYSTEMS
Chernaya M.M.
1 - 37 of 37 Items

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