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The concept of generalized method of calculation and design of wet cleaning duct GTD
Silaev B.M., Malcev E.N.
Diagnostics of state gas-fluid of flows in the field of cross vibration
Limanova N.I., Levkin U.S.
Technology of computational analysis of the working process parameters of low-thrust rocket engines running on gaseous oxygen-hydrogen fuel with the use of ANSYS CFD
Ryzhkov V.V., Morozov I.I.
Application of open-source software for industrial problems of vehicle lift-off gas dynamics
Abdurashidov T.O., Osipov A.V., Korchagova V.N., Kraposhin M.V., Smirnova Y.V., Strizhak S.V.
Micro gas turbine engine imitation model
Kuznetsov A.V., Makaryants G.M.
Using the «virtual engine» software in automatic control system of gas turbine engine
Golberg F.D., Gurevich O.S., Petukhov A.A.
Determination of relative position and orientation of nanosatellites by video image analysis
Simakov S.P., Ustyugov E.V.
Dynamic modelling of non-linear vibrations in cylindrical tooth gearing of aircraft drive systems
Kalinin D.V., Temis J.M.
Model and algorithm of short-term planning of industrial activity of the enterprise in the context of heterogeneous polypoly
Bogatyrev V.D., Levitan V.G.
Research of small spacecraft dynamiсs taking into account the influence of elastic vibrations of asjacent solar panels and aerodynamic moment
Yelenev V.D., Titov B.A., Davydov E.I., Davydov I.E., Kochyan A.G., Yudintsev V.V.
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.
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.
The formation of the contoured surface roughness level of optical purity by using a CNC machine
Abulkhanov S.R., Sazonov M.B.
Dynamic process modeling of aircraft engine control system
Blyumin K.V.
Conceptually logical model of an integrated data system (software & hardware) for the control of individual and small-scale production of aviation components
Prilepsky I.V.
Numerical study of gasdynamic characteristics counterflow burner with use of anisotropic models of turbulence
Piralishvily S.A., Guryanov A.I., Badernikov A.V.
Research of gasodynamic seal characteristics under transient conditions of aircraft engines and power plants
Vinogradov A.S.
Economic-mathematical model of system of monetary stimulation of workers of the special mechanical engineering enterprise
Ivanov D.U.
Mathematical modelling of the content of electronic educational resources
Solovov A.V.
Improving the operating characteristics of engines by the imposition of manufacturing operation of hermeticity inspection of vacuum-tight radio electronic device cases
Electronic model of turbine drive flow for its direct optimization
1 1.
Comparative analysis of different approaches to designing thin-walled element structures of composite materials
Komarov V.A., Tchernyaev A.V.
The process of ice formation on the surface of cryogenic tanks
Biryuk V.V., Shepelev A.I.
Structural model of individual forecasting of space radioelectronic equipment parameters
Tyulevin S.V., Piganov M.N.
Model of economic cooperation between an air carrier and airport structures
Titov B.A., Kropiventseva S.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.
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.
Physical workflow model in the combustion chamber LREST with a jet-centrifugal jets on hypergolic propellants
Silyutin M.V., Shustov S.A.
Mathematical model of mastering educational information of the academic process
Titov B.A., Ryabinova E.N.
Simulation of turbulent flow in simple and complex diffuser channels
Davletshin I.S., Mingazov B.G., Yavkin V.B., Kesel B.A., Voskoboynikov D.V.
Set-theory model of the aircraft hydraulic system working fluid state
Koptev A.N., Gareyev A.M., Popelnyuk I.A.
Control over the deployment of an orbital tether system of great length
Wang C., Zabolotnov Y.M.
Analisys of the influence of radial displacement of a particle on the parameters of an eddy-current probe
Gudkov S.A., Kudryavtsev I.A.
System-mathematical simulation of engine air hydraulic power supply
Goryunova N.R., Goryunov A.A.
Approximation of characteristics of linear displacement inductive sensors using modified Gaussian function with a first order difference argument
Tingaev V.S., Matyunin S.A., Mednikov V.A.
Simulation of aerodynamic structure of the flow in the combustion chamber of a small-size gas turbine engine with the help of CAE–systems
Matveev S.G., Orlov M.Y., Abrashkin V.Y., Zubrilin I.A., Matveev S.S.
Model of managerial decision making by enterprise of the trade and marketing network in collaboration with the industrial complex
Astapov S., Bogatyrev V.D.
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.
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.
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.
A model of monitoring the demand function in the context of a polipoly with the "ASK-RENTGEN" enterprise taken as an example
Bogatyrev V.D., Levitan V.G.
Methodology systems approach in models of technological subassembly in the aircraft industry
Barvinok V.A., Tlustenko S.F.
The development of mathematical models of acoustic characteristics of the elastic porous material «metal-rubber»
Safin A.I., Igolkin A.A.
Mathematical model and peculiarities of operating mobile robots with hybrid drives
Ilyukhin Y.V., Tatarintseva A.V.
Simulation and research of factors affecting aerodynamic indices of the gas purification process
Usmanova R.R., Zhernakov V.S.
Analysis of the terminological status of the «overall cost» concept (methodological aspect)
Sosnina T.N.
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.
Investigation of extreme opportunities of stand supporting systems
Samsonov V.N., Kozyreva M.S., Cherevan A.A.
Method of improving control using a simulation object model and its application to the problem of helicopter emergency landing manoeuvre optimization
Kvokov V.N., Trushkova Y.A., Ukhin M.Y.
Model of varigrained particle stream moving by hypersonic combustion materials investigation
Bulanova E.A., Pervishin A.N.
Identification of a gas turbine engine mathematical model by the ressults of testing
Botchkaryov S.K., Dmitriyev A.Y.
Optimal design of an induction heater of minimum length
Mednikova V.A.
Verification of a design model and evaluation of a technique of manufacturing aircraft engine composite parts on the basis of dynamic tests
Zinin A.V., Arkhipov A.N., Kholobtsev D.P., Ravikovich Y.A., Shevjakov A.O., Kholmanova M.A.
Design build process for the accuracy of eligibility
Grechnikov F.V., Tlustenko S.F.
3D-model of compressor rotor blade development
Boyarov K.V., Ryazanov A.I., Chempinsky L.A.
Sales training methods based on through the use of CAD / CAM / CAE systems for aero engines
Balyakin A.V., Ermakov A.I., Pronichev N.D., Chempinsky L.A.
Process of coating the inner surface of an inclined pipe and its mathematical modeling
Skvortsov B.V., Zaretskaya M.I., Zaretskiy I.S., Zhivonosnovskiy P.A.
Estimation of functional efficiency of the air transport service system at a regional airport terminal
Koltsov I.V., Romanenko V.A.
Mathematical models of squeeze film dampers in rotor dynamics of gas turbine engines
Kutakov M.N., Degtiarev S.A., Leontiev M.K.
Spacecraft power supply system using additional low-power sources of energy
Kargu D.L., Beznyakov A.M., Nemirov A.V.
Analysis of the effectiveness of predictive models of quality parameters of the chips
Tyulevin S.V., Arhipov A.I., Piganov M.N., Elizarov S.V.
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.
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.
Validation of CFD-models of gas turbine engine uncooled turbines
Matveev V.N., Popov G.M., Goryachkin E.S., Smirnova Y.D.
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.
Stabilization of a pilot-operated gas pressure control valve by placing a throttle at the inlet
Stadnik D.M., Sverbilov V.Y., Makaryants G.M., Makaryants M.V.
Improving the high pressure compressor efficiency by optimizing the stator blades angles
Popov G.M.
Additive technology application details of combustion
Balyakin A.V., Smelov V.G., Chempinskiy L.A.
Simulator, algorithm and software for the computation of differential gas circuits frequency response
Igonin A.A., Gimadiev A.G.
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.
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.
Working out the system of technical decisions for ensuring the reliability of friction units of gas-turbine engines
Gromakovsky D.G., Kovshov A.G., Ibatullin I.D.
Laser optico-acoustical octane meter in systems of optimizing the process of commercial petrol compound-filling
Astapov V.N.
Development of the information technology for estimation of fundus image geometric parameters
Kuprijanov A.V., Ilyasova N.Y.
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.
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.
Investigation of resonant oscillations working plates in experimental models of pneumatic valve
Zhuravliov О.A., Komarov S.Y., Makaryants G.M., Sergeev R.N., Harchikova J.V.
Modeling of heat conduction process in porous MR material
Zhizhkin A.M.
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.
Prospective lines of improving the process of evaluating the technical condition of aircraft hydraulic system working fluid
Koptev A.N., Gareyev A.M., Popelnyuk I.A.
Using apriori information in interferometric processing of high resolution sar data
Ushenkin V.A., Egoshkin N.A.
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.
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.
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