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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.
Developing models of information-analytical monitoring system design, engineering and manufacturing processes aircraft companies
Zheleznov O.V., Blyumenshteyn A.A., Chernikov M.S.
Methodology for assessing and reducing the aerodynamic imbalance of the impellers of GTE fans
Kudashov E.V., Grachev I.A., Bolotov M.A.
Development of automated systems LC UPD
Blyumenshteyn A.A., Chernikov M.S., Zheleznov O.V.
Optimization of operation mode and design parameters of a finely-dispersed metallic liquid-alloy generator
Egorychev V.S., Ryazanov A.I., Khaimovich A.I.
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.
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.
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.
Assessment of the endurance limit of light structural metal components using the fatigue surface development method
Zalyaev R.A., Kirpichev V.A.
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.
Automation of the process of testing on-board systems of unmanned aerial vehicles
Kirillov A.V., Sitnikov V.V., Tuchin A.L.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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