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Optimal design of an induction heater of minimum length
Mednikova V.A.
Kinetic model and kerosene surrogate for calculating gas turbine engine emission of carcinogenic hydrocarbons
Semenikhin A.S., Idrisov D.V., Chechet I.V., Matveev S.G., Lukachev S.V.
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.
Simulation model of oscillations of the “sun gear – satellites” pair of turboprop engine planetary reduction gearbox in the presence of defects of tooth flanks
Kryuchkov A.N., Plotnikov S.M., Sundukov E.V., Sundukov A.E.
Forces distribution in thread and external altering load factor in thread joint under structures vibration
Kurushin M.I., Kurushin A.M., Barmanov I.S.
Physical workflow model in the combustion chamber LREST with a jet-centrifugal jets on hypergolic propellants
Silyutin M.V., Shustov S.A.
Turboprofan jet modeling and equivalent specific fuel consumption optimization subsystem construction on the seminatural modelling stand
Pogorelov G.I., Krivosheev I.A., Godovanyuk A.G., Danilin O.E., Badamshin B.I.
Development of methods for ensuring energy balance for the operation of mission equipment of “AIST”-series small satellites under conditions of power limitations
Ivanushkin M.A., Salmin V.V., Tkachenko S.I., Tkachenko I.S., Volgin S.S.
Peculiarities of using additional low-power energy sources in the power supply system of small spacecraft
Kargu D.L., Beznyakov A.M., Nemirov A.V., Radionov N.V., Chudnovsky Y.A.
Frequency characteristics of a coaxial gas damper for booster feed line
Odinokov D.A., Gimadiyev A.G.
Study of uncertainty of measuring geometrical parameters of gas turbine engine compressor blade profiles
Pechenin V.A., Bolotov M.V., Ruzanov N.V., Yanyukina M.V.
Method of accelerated test research soldered joints surface mount devices
Nasedkin A.V.
Simulation of wire manufacturing production cycle
Haymovich I.N., Skripachyov D.G., Kolesnikova S.Y.
Modeling of propane combustion processes in case of converting a GTE combustion chamber to gaseous fuel
Matveev S.G., Lanskiy A.M., Orlov M.Y., Abrashkin V.Y., Dmitriev D.N., Zubrilin I.A., Semenov A.V.
Functional components of the model of pedagogical activity of a distance learning teacher
Belousov A.I., Gromova T.V.
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.
Development of a mathematical model of winding made of non-impregnated aramid fibers for strength analysis of the combined fan case in GTE compressor blade separation
Krundaeva A.N., Shmotin Y.N., Tomilina T.V.
Conceptual model of the formation of flying skills in the process of training using flight simulators
Godunov A.I., Kuatov B.Z., Yurkov N.K., Kurtaev S.Z.
Models of competitive interaction between enterprises and formation of parametrically stable equilibrium states
Grishanov G.M., Kolychev S.A., Klentak L.S.
Analysis оf the cutting force of heat resisting alloys during high-speed milling
Khaimovich A.I., Kuznetsov A.V.
Simulating of Roots compressor
Belov G.O., Ermilov M.A., Kryuchkov A.N.
Technological processes simulation incomplex parts production of aerospacetechnical equipment: problems and the ways of their solving
Bolotov M.A., Zhidyaev A.N., Surkov O.S.
Method of compression of digital halftone images on the basis of markov chains with several states
Petrov E.P., Harina N.L., Rzhanikova E.D.
Classification of models of basic links in the air transport sector in the context of the process of macrologistic system formation and development
Pakhomov A.A.
Reduction of circumferential variation in the final stage of IPC
Baturin O.V., Krivcov A.V., Matveev V.N., Popov G.M.
Calculation of hydrodynamic noise in the diffuser of a pulsation damper flow channel
Makaryants G.M., Gafurov S.A., Zubrilin I.A., Kryuchkov A.N., Shakhmatov Y.V., Berestovitsky E.G., Gladilin Y.A.
Questions of economic justification converting aviation engines for use in compressor stations of unified gas supply system
Vorobyov M.Y.
Using active noise suppression non-adaptive systems with a transfer function model for the reduction of medical equipment noise
Sementsov S.G.
The development of mathematical model of hydrodynamics of "tpapped" volume in the gear pump
1 1., 1 1., 1 1., 1 1., 1 1.
Simulation of the distributed selection and supply of cooling air in gas-turb engine
Goryunov A.I., Goryunov I.M.
Simulation of automatic systems of controlling space vehicle drives
Zhuravlyova Y.V.
Methods and models of autonomous control over Earth remote sensing spacecraft survivability
Akhmetov R.N.
Experimental and design analysis of models of cyclic compression for a multilayer multispan package of corrugated sheets
Eskin I.D., Alkeev R.I., Ivashchenko V.I.
Correlation and regression model for the assessment of circular non-uniformity of the gas temperature field at the outlet of small gas turbine engine combustion chambers
Lukachev S.V., Abrashkin V.Y., Lansky A.M., Matveev S.G.
Aspects of the numerical method calculating thermogazodynamic lrest based on not perfect passing of workflows in the combustion chamber
Silyutin M.V., Shustov S.A.
3D-model of compressor rotor blade development
Boyarov K.V., Ryazanov A.I., Chempinsky L.A.
Calculation of indicator diagram dynamic test at internalcombustion engine in KDAM environment
Kosenok B.B.
Оptimization of gas turbine aircraft engine control throughout the engine service life
Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.
Influence of turbulence models on calculated values of aircraft aerodynamic properties
Elisov N.A., Ishkov S.A., Shakhov V.G.
Optimization of parameters of a hub aircraft ground handling system on the basis of a fuzzy-controller simulation model
Vasileva I.A., Romanenko V.A., Khvostova T.V.
Application of simulation modelling in static tests of space-rocket vehicles
Grebnev D.N., Duplihin V.K., Zuperman J.A., Aistov A.I., Kukushkin V.E.
Quality forecasting solder joint electronic components
Shumskikh I.Y.
Method of creating digital terrain models and its practical application as exemplified by Samara region
Anshakov G.P., Myatov G.N., Malinovskii V.A.
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.
Functional chart of a multichannel hydrologic-optical-chemical measuring complex and new measuring channels of hydrophysical parameters
Smirnov G.V., Olenin A.L.
Formation of spread in resonance stresses in bladed disks with non-identical blades and loose vibration conectedness
Ermakov A.I., Urlapkin A.V., Fedorchenko D.G.
Latest investigations on underplatform damper inner mechanics
Gola M.M., Gastaldi C.
Analysis of models of fuel elements while using of surface mountng
Knyazeva G.N., Krasnoshchekova G.F., Tyulevin S.V.
Parameters study in the electrothermal and jet protection of the airliner cockpit windows from fogging
Nikolayev V.N.
Linear mathematical model for the determination of rational treatment conditions on the finishing end milling operations in the manufacture of aircraft parts
Skuratov D.L.
Simulation of manufacturing processes within the concept of «lean production»
Smelov V.G., Kokareva V.V., Shitarev I.L.
Dynamic process modeling of aircraft engine control system
Blyumin K.V.
Simulation of ultrashort pulse transmission in a chain of fused silica microspheres
Kozlova E.S.
A hot-wire anemometric transducer of airflow mass rate
Nikolayev V.N.
Optimization of strength characteristics of lighting devices aircraft by construction of virtual models
Abulkhanov S.R., Goryainov D.S., Skuratov D.L.
Modeling static and dynamic characteristics of pressure reducing valves
Igolkin A.A.
Calculating the parameters of eddy current converters when testing several samples of cylindrical shape
Gainullina G.M., Polulekh A.V.
Approach to the assessment and forecasting for onboard computer systems of monitoring space vechiles during its usage based on full-scale experiments
1 1., 1 1., 1 1.
Hemispherical high-speed particle transducer
Izyumov M.V., Syomkin N.D.
Experimental acknowledgement of adequacy of the developed mathematical model of instant giving of the liquid by the gear pump
1 1., 1 1., 1 1., 1 1., 1 1.
Increase of stability of technological systems at processing of details aircrafts engines
Skuratov D.L., Burmistrov E.V., Samykin V.N.
Development of the finite element model of vibroacoustical characteristics of pipe system
Mironova T.B., Prokofiev A.B., Shahmatov E.V.
3D model didactic properties investigations for geometrical modeling principles training
Ivashchenko V.I.
Verification of a complex of mathematical models of aerodynamics and dynamics of Savonius rotor motion
Sizov D.A., Onushkin Y.P., Krasnova O.A., Dzhanibekov O.T.
Study of the mechanism of flame stabilization in aaluminum-air mixture
Egorov A.G., Tizilov A.S.
Mathematical model for calculating pressure in a pulsating combustion chamber
Solodovnikov A.V., Odentsov D.A., Kravtsov E.V., Golubyatnik V.V., Shcheblykin D.A.
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.
Use of probability distribution mixes in airport simulation model
Romanenko V.A.
Design build process for the accuracy of eligibility
Grechnikov F.V., Tlustenko S.F.
Modeling of heat conduction process in porous MR material
Zhizhkin A.M.
Experimental and theoretical research of continuous motion of rotor on anisotropic gapped elastic support
Nikiforov A.N., Panovko G.Y., Shokhin A.Y.
Schemes, parameters, work process, characteristics and structure of long-range interception aircraft engines
Kovalev A.V., Sanin V.N., Krivenok A.G., Korolenko V.V.
Constructing 3D fan blade models in CAD-system on the basis of coordinate measuring techniques
Arkhipov A.N., Ravikovich Y.A., Fedorov I.M., Kholobtsev D.P.
Mathematical model of surface layer formation during hydroabrasive jet machining
Meshcheryakov A.V., Shulepov A.P.
Uniform access to universal data storage
Yablokov D.E.
Mathematical modeling of technological production process of thermo-stable resistor – capacity structures
Merkulov A.I., Laktanov P.V., Merkulov V.A.
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.
Problems of design analysis of characteristics of a gas turbine engine working on natural gas
Gulina S.A., Orlov M.Y., Mikheyenkov E.L.
ASMTurbC method of autonomous statistical modeling of diffusion turbulent combustion and the results of its testing
Nuzhnov Y.V.
Development of the technology of diagnostics of turbo-jet aviation engines by a filtering element with a diagnostic layer
Drokov V.V., Drokov V.G., Muryshenko V.V., Mukhutdinov F.I., Khaliullin V.F.
Modeling of stall cavitation sensitivity of a booster turbopump assembly and comparison between experimental and numerical results
Kazyonnov I.S., Kanalin U.I., Poletaev N.P., Chernisheva I.A.
Method of production testing of electronic parts
Nasedkin A.V., Tyulevin S.V., Piganov M.N.
Analysis of the cause of serious flight accident
Vakhrushev D.E., Agaphonov O.A., Pryadko S.P., Schukin A.V.
Introduction of model-based approach to design aircraft
Agaphonov O.A., Vakhrushev D.E., Pryadko S.P., Schukin A.V.
3d virtual simulation and casting process optimization of part GTE "Swirler of II duct" with using computer technologies
Vdovin R.A.
The development of mathematical models of acoustic characteristics of the elastic porous material «metal-rubber»
Safin A.I., Igolkin A.A.
Universal approach to the description of working medium chambers for simulating hydraulic and pneumatic systems
Timofeyev Y.M., Khalatov E.M.
Research of the process of sheet presswork using polyurethane under constrained bending
Eskina E.V., Gromova E.G.
Automated generation of structural members of a spacecraft thermal model
Kulikov D.S., Shatin A.A., Velmisov I.G.
Method of reducing design aerodynamic characteristics to the results of drain tests of a transport category aircraft model
Bondar Y.I.
Theoretical and experimental analysis of the thermal state of transport aircraft compartments thermal state
Nikolayev V.N.
Methods of measurement and calculation of microaccelerations onboard of low orbit space microgravitational platform
1 1., 1 1., 1 1.
Plane high-speed particle transducer
Izyumov M.V., Syomkin N.D.
The simplification of heat engines thermodynamics calculation with using of idaeal gas’ model
1 1., 1 1.
Invariancy of vector models in modelling tooth gearings
Kosenok B.B.
A model of motion of monodispersible gas-liquid stream is in transzvukovoy of part of rocket chamber
Еpishchenko S.V., Pervishin A.N.
Dissipative structures of the Gierer-Meinhardt model of morphogenesis in the stochastic field
Kurushina S.E.
Simulation modeling as a method of assessing the resource intensity of space rocket complex support equipment operation
Shcherbina I.S.
Three-dimensional periodic thermoelastichydrodynamic modeling of hydrodynamic processes of a thrust bearing
Sokolov N.V., Khadiev M.B., Fedotov P.E., Fedotov E.M.
Acoustic diagnostics of local damages of spur wheels in multi-shaft drive using neural network models
Parfiyevich A.N., Dragan A.V., Sokol V.A.
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