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Comparison of quasi-three-dimensional and full three-dimensional formulations of thrust bearing operation
Sokolov N.V., Khadiev M.B., Fedotov P.E., Fedotov E.M.
Modal analysis of a spacecraft solar panel
Kryuchkov A.N., Safin A.I., Ermilov M.A., Vidyaskina A.N., Igolkin A.A., Ye. V. Shakhmatov Y.V.
Digital model of the drag force of the Earth’s upper atmosphere for the design of low-orbit spacecraft
Volotsuev V.V.
Numerical method for determining the parameters of a creep curve on the basis of Soderberg law
Makarov R.Y.
Methodology for assessing and reducing the aerodynamic imbalance of the impellers of GTE fans
Kudashov E.V., Grachev I.A., Bolotov M.A.
Developing models of information-analytical monitoring system design, engineering and manufacturing processes aircraft companies
Zheleznov O.V., Blyumenshteyn A.A., Chernikov M.S.
Optimization of operation mode and design parameters of a finely-dispersed metallic liquid-alloy generator
Egorychev V.S., Ryazanov A.I., Khaimovich A.I.
Development of automated systems LC UPD
Blyumenshteyn A.A., Chernikov M.S., Zheleznov O.V.
Leader competition in biological and social systems
Pivovarova A.S., Steryakov A.A.
Model of virtual balancing of rigid rotors
Khaimovich A.I., Bolotov M.A., Pechenina E.Y.
Determination of loads on perforated tank partition
Filipov A.G., Glazkov I.E.
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.
Mathematical model of training and self-training in maintenance of complicated systems
Koptev A.N., Popovich A.A.
Development of an experimental plant and a numerical model of an axial magnetic rotor suspension
Benedyuk M.A., Lomachev A.O., Badykov R.R., Bezborodova K.V., Yurtaev A.A.
Numerical method of determining creep model parameters within the first two stages of creep
Zoteev V.E., Makarov R.Y.
Heat exchange parameters of units and pipelines of the aircraft hydraulic system
Nikolayev V.N.
Methodology complex of hardware-in-the-loop functional modelling of gas turbines and its systems
1 1., 1 1., 1 1., 1 1., 1 1.
Development of a structural and algorithmic model of pur-poseful actions of experts in maintenance and repair
Koptev A.N., Popovich A.A.
Neural network controller of a gas turbine plant low emission combustor
Avgustinovich V.G., Kuznetsova T.A., Sukharev A.A.
Model for evaluating the end runouts of a rotor with parallel connections of parts
Grachev I.A., Kudashov E.V., Bolotov M.A., Pronichev N.D.
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.
Modal analysis of the dynamic mockup of “AIST–2D” small spacecraft
Igolkin A.A., Safin A.I., Filipov A.G.
Verification of aero-engine numerical rotor models based on virtual static structural and modal tests
Shaposhnikov K.V., Degtyarev S.A., Leontiev M.K., Anisimov S.V.
Forecasting technique of semiconductor diodes quality indicators
Kozlova I.N., Tyulevin S.V., Tokareva A.V.
Development of a multiparameter model of an optimum coherent system of incentives for workers of aircraft construction enterpricses
Ivanov D.Y.
Models of economic agents’ interaction in conditions of an asymmetric information structure
Yakunin A.M.
Mathematical model of a generalized quadcopter kinematic scheme and its software implementation
Zelenskiy V.A., Kovalev M.A., Ovakimyan D.N., Kirillov V.S.
Approximate models of air transport queueing systems with partial mutual assistance between service channels
Romanenko V.A.
Method of producer 3D parametric models of sample parts in SIEMNES NX
Goryachkin E.S., Rjazanov A.I., Urlapkin A.V., Chempinskiy L.A.
Comparative analysis of turbulence model influence in numerical simulation of an experimental radial compressor stage
Eremenko V.V., Mikhailov A.E., Mikhailova A.B., Goryukhin M.O., Krasnoperov D.G.
Simulation design, kinematic and dynamic analysis of "virtual piston engine"
Gvozdev A.S., Melentjev V.S.
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.
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