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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.
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.
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.
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.
Design of experiments for verification of computational life prediction methods
Samsonova O.V., Fetisov K.V., Karpman I.V., Burtseva I.V.
Dataware of virtual lab for gas turbine engine testing
Rybakov V.N., Kuzmichev V.S., Kulagin V.V., Krupenich I.N., Fedorov D.V.
Dynamik experimental researches of the face gas dynamic seal
Novikov D.K., Balyakin V.B., Sedov V.V.
Ensuring permissible level of gas turbine dynamic loading in operation by means of standard engine control devices
Chervonyuk V.V., Korovin B.B.
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.
Build-up mathematical model of allocation temperature gas along an axis the channel a torch discharge at interaction with thick-film devices of microassambly
Stolbikov A.V., Piganov M.N., Kostin A.V.
Research of hydrodynamic processes in the lubrication system of gas turbine engines
Gulienko A.I., Shchurovskiy Y.M.
Optimization model of financing production of an industrial enterprise of space-rocket industry
Inozemtsev V.V.
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.
Computer-aided system of virtual gas turbine engine testing
Tkachenko A.Y., Rybakov V.N., Krupenich I.N., Ostapuk Y.A., Filinov E.P.
The influence of the shuttle effect on the intensification of heat losses in a Stirling engine
Savchenko V.A., Stolyarov S.P.
Real-time control algorithms requirements verification mathematical model implementation in visual design computer-aided system
Shulyndin A.V., Tjugashev A.A.
Information support of aviation embedded information and control systems lifecycle
Akimova T.E.
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.
The formation of the contoured surface roughness level of optical purity by using a CNC machine
Abulkhanov S.R., Sazonov M.B.
Additive technology application details of combustion
Balyakin A.V., Smelov V.G., Chempinskiy L.A.
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.
Analysis of random uncertainties of heart rate variability
Fedotov A.A., Akulova A.S., Akulov S.A.
Constructing the specification for the on-board realtime control algorithm
Tyugashev A.A., Bogatov A.Y.
Analysis of on-board equipment robustness on the basis of COTS-products
Yefanov V.N., Bondarev A.V.
Rail line models for adaptive receiver track circuits
1 1.
Methodology of the adaptive graphic and geometric training for the computer aided design teaching
1 1.
Modeling of heat conduction process in porous MR material
1 1.
Reputation of enterprises competing in the market from the point of view of consumers
Ivanov D.Y., Kirilina Y.V.
Perfection of technological preparation of manufacture of blades of compressor GTD on the basis of use of parametrical models
Orlov R.R., Pronichev N.D., Chempinsky L.A.
Models and algorithms of choosing solutions on search iterations in numerical vector schemes
Belokurov S.V.
Verifying models of mechatronic systems «man-centrifuge» for ground and space usage on the basis of set theory
Anshakov G.P., Akulov V.A., Balakin V.L.
Influence of the reliability of Earth remote sensing spacecraft onboard systems on the monitoring of imaging periodicity
Kirilin A.N., Akhmetov R.N., Kurenkov V.I., Kapitonov V.A., Stratilatov N.R., Lokhmatkin V.V.
Digital design of heat-resistant dimensionally stable carbon laminate (CFRP) structures
Komarov V.A., Kishov E.A., Laikova O.G., Pavlov A.A.
Method of calculating dynamic designs of space launch vehicles for designing systems of stabilization of their motion
Lobanov V.A.
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.
Investigatiom of interrelation of gluing designs defects from polymeric composite materials
Mordasov V.I., Storozh A.D., Grebnev N.E., Grebnev D.N., Shulepova O.V.
Numerical study of possibility of reliable diagnostics of gas turbine engine by gasdynamic parameters using a linear mathematical model
Gerasimov A.B., Sundukov M.Y.
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.
Peculiarities of using hot-air balloons in tests of parachute systems
Kurinny S.M., Krivorotov M.M., Baranichenko E.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.
Dynamic modelling of non-linear vibrations in cylindrical tooth gearing of aircraft drive systems
Kalinin D.V., Temis J.M.
Study of characteristics of the launch vehicle fuel line gas damper
Gimadiev A.G., Odinokov D.A., Stadnik D.M., Greshnyakov P.I.
Research of machinability of heat resistant steels 10Х11НN23T3MР-ВД used in parts of gas turbine engines
Surkov O.S., Kondratiev A.I., Alexeev V.P., Haymovich A.I.
CFD-modeling of processes in a high-pressure oxidizer pump for the turbopump assembly of a liquid rocket engine
Zubanov V.M., Shabliy L.S.
Comparison of mathematical simulation results and experimental research of PVD-K3-1 air pressure probe
Moiseev V.N., Dubinina M.M., Pavlovsky A.A., Sorokin M.Y.
Automated construction of a 3D plane model at the stage of technical proposals
Borgest N.M., Aleev R.H., Aksanian P.A., Gromov A.A.
Methodology systems approach in models of technological subassembly in the aircraft industry
Barvinok V.A., Tlustenko S.F.
Calculation methodology of intermittent burning chamber main parameters
Solodovnikov A.V., Vishegorodcev E.N., Golubyatnik V.V.
Mathematical model and peculiarities of operating mobile robots with hybrid drives
Ilyukhin Y.V., Tatarintseva A.V.
Definition of overall limits internal-combustion engine using vector modeling
Kosenok B.B.
Estimation of the adequacy of electronic flow model and efficiency characteristic of small centripetal turbine drive
Matveev V.N., Shabliy L.S.
Some features of nonlinear interaction of vibration modes of thin circular cylindrical shells
Taranukha N.A., Leyzerovich G.S.
Model of electromigration in thin metal films
1 1., 1 1.
Conception of the student work place arrengement for the computer aided design base teaching
1 1., 1 1.
Modeling of structure of the porous MR material in process of heat conduction
1 1.
Comparative analysis of different approaches to designing thin-walled element structures of composite materials
Komarov V.A., Tchernyaev A.V.
Ways 3D parametrization TJ blades for use CAD/CAM/CAE packages
Smelov V.G., Shitarev I.L.
Modelling changes of condition of aircraft hydraulic system working fluid
Gareyev A.M.
Model of economic cooperation between an air carrier and airport structures
Titov B.A., Kropiventseva S.A.
Influence of deviations in manufacturing of electrothermal propulsion system on nanosatellite maneuvering accuracy
Sinitsin L.I., Belokonov I.V.
Fuzzy-controller simulation model as a tool of optimization of a limited availability ground handling system at a hub airport
Romanenko V.A.
Theoretical and experimental investigation of the photographic reconnaissance plane instrument bay thermal state
Nikolayev V.N.
Laser-vibrating method for testing of gluing designs from polymeric composite materials
Mordasov V.I., Storozh A.D., Grebnev N.E., Grebnev D.N., Shulepova O.V.
Diagnostics of state gas-fluid of flows in the field of cross vibration
Limanova N.I., Levkin U.S.
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.
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.
Influence of the suspension system on the accuracy of the aircraft modal testing results
Berns V.A., Dolgopolov A.V., Zhukov E.P., Marinin D.A.
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