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Authors
Digital model of the drag force of the Earth’s upper atmosphere for the design of low-orbit spacecraft
Volotsuev V.V.
Methodology for assessing and reducing the aerodynamic imbalance of the impellers of GTE fans
Kudashov E.V., Grachev I.A., Bolotov M.A.
Numerical method for determining the parameters of a creep curve on the basis of Soderberg law
Makarov R.Y.
Optimization of operation mode and design parameters of a finely-dispersed metallic liquid-alloy generator
Egorychev V.S., Ryazanov A.I., Khaimovich A.I.
Developing models of information-analytical monitoring system design, engineering and manufacturing processes aircraft companies
Zheleznov O.V., Blyumenshteyn A.A., Chernikov M.S.
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.
Improving the accuracy of industrial robot movements in the process of incremental shaping
Sazonnikova N.A., Ilyukhin V.N., Surudin S.V., Mezentsev D.A.
Compressor blade erosion modeling
Gumerov A.V., Akmaletdinov R.G.
Investigation of the dynamic characteristics of the pneumatic-mechanical drive of the installation movements of machine mechanisms
Prikhodko S.P., Sidorenko V.S., Korotych D.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.
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.
Automation of the process of testing on-board systems of unmanned aerial vehicles
Kirillov A.V., Sitnikov V.V., Tuchin A.L.
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.
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.
Models of economic agents’ interaction in conditions of an asymmetric information structure
Yakunin A.M.
Method of producer 3D parametric models of sample parts in SIEMNES NX
Goryachkin E.S., Rjazanov A.I., Urlapkin A.V., Chempinskiy L.A.
Mathematical model of training and self-training in maintenance of complicated systems
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.
Automatization of creation vane 3D-model in Ansys TurboGrid with geometry data in traditional view
Dmitrieva I.B., Shabliy L.S.
Numerical method of determining creep model parameters within the first two stages of creep
Zoteev V.E., Makarov R.Y.
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.
Simulation design, kinematic and dynamic analysis of "virtual piston engine"
Gvozdev A.S., Melentjev V.S.
Development of a structural and algorithmic model of pur-poseful actions of experts in maintenance and repair
Koptev A.N., Popovich A.A.
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.
Modal analysis of the dynamic mockup of “AIST–2D” small spacecraft
Igolkin A.A., Safin A.I., Filipov A.G.
Development of a multiparameter model of an optimum coherent system of incentives for workers of aircraft construction enterpricses
Ivanov D.Y.
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.
Forecasting technique of semiconductor diodes quality indicators
Kozlova I.N., Tyulevin S.V., Tokareva A.V.
Development of automated systems LC UPD
Blyumenshteyn A.A., Chernikov M.S., Zheleznov O.V.
Parametric identification of coefficients for a model of fatigue stiffness degradation of a composite material
Panteleev A.V., Turbin N.V., Nadorov I.S., Kononov N.O.
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.
Mathematical model of anisotropic elastic-plastic material
Grechnikov F.V., Yerisov Y.A.
Automatization of creation vane models for CAE with PROFILER
Shabliy L.S., Dmitrieva I.B., Popov G.M.
Leader competition in biological and social systems
Pivovarova A.S., Steryakov A.A.
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.
Dynamic of the a safety vent valve
Makaryjants M.V., Kudyurov L.V., Mustafaev Y.K., Tumanov D.V.
The influence of the shuttle effect on the intensification of heat losses in a Stirling engine
Savchenko V.A., Stolyarov S.P.
Optimization of model positional harakterstik of the electromagnetic sensor of the linear peremeshchny
Tingaev V.S., Matyunin S.A., Mednikov V.A.
Information support of aviation embedded information and control systems lifecycle
Akimova T.E.
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.
Test of kinematic model by pneumatic manipulator
Gribkov A.M., Shilin D.V., Filin I.P.
Calculation methodology of intermittent burning chamber main parameters
Solodovnikov A.V., Vishegorodcev E.N., Golubyatnik V.V.
Mathematical modeling of heat exchange on air cooling of a number of aluminum ingots
Gorshenin A.S.
Optimization of aircraft seven stage compressor first stages parameters
Popov G.M., Matveev V.N., Baturin O.V., Kolmakova D.A.
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.
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.
Formation of a structural calculated mesh the passage blade of the axial turbine in program GAMBIT
Baturin N.V., Baturin O.V., Matveev V.N.
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.
Mathematical modeling of dynamic processes in a hydraulic drive with a discrete regulator of liquid flow
Shakhmatov Y.V., Gimadiev A.G., Sverbilov V.Y., Sinyakov A.F.
Study of the mechanism of flame stabilization in aaluminum-air mixture
Egorov A.G., Tizilov A.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.
Flexible geometrical model of pipeline
Gavrilov V.N.
Concept of construction of virtual lab for gas turbine engine testing
Rybakov V.N., Kuzmichev V.S., Tkachenko A.Y.
Aircraft engine design based on unified gas generator
Vinogradov A.S., Parovay Y.F., Mordvinov A.G., Popov D.V., Shirokov M.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.
Frequency characteristics of a coaxial gas damper for booster feed line
Odinokov D.A., Gimadiyev A.G.
Method of lossless image compression in the Earth remote sensing systems
Petrov E.P., Kharina N.L., Sukhikh P.N.
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.
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.
Computer-aided system of virtual gas turbine engine testing
Tkachenko A.Y., Rybakov V.N., Krupenich I.N., Ostapuk Y.A., Filinov E.P.
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.
Real-time control algorithms requirements verification mathematical model implementation in visual design computer-aided system
Shulyndin A.V., Tjugashev A.A.
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.
Experimental research of vibrations of pipeline of GTD with support from MR for working off method of calculation in environment of ANSYS
Shvetsov A.V., Lezhin D.P., Ulanov A.M.
The parameters of turbulence models and grids investigation on CFD results of plane turbine cascade
Zubanov V.M., Krivcov A.V., Shtraub A.A.
Linear mathematical model for the determination of rational treatment conditions on the diamond smoothing operations in the manufacture of aircraft parts
Skuratov D.L., Shvetsov A.N., Abulkhanov S.R.
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.
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.
Mathematical model of an eddy current converter for testing discontinuous structure samples
1 1., 1 1.
Extrapolation of conditions of an information measuring and control system with the iterative algorithm of operation
Zelensky V.A.
Simulation of the distributed selection and supply of cooling air in gas-turb engine
Goryunov A.I., Goryunov I.M.
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.
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