Calculation of optimum transfers from high-elliptic orbits to geostationary orbits using a stationary plasma engine
Kvetkin A.A., Kolesov A.V.
Comparative analysis of different approaches to designing thin-walled element structures of composite materials
Komarov V.A., Tchernyaev A.V.
Method of individual selection of parts for selective assembly of electrohydraulic servo drives
Medvedev A.V., Khalatov E.M.
Optimization of operation mode and design parameters of a finely-dispersed metallic liquid-alloy generator
Egorychev V.S., Ryazanov A.I., Khaimovich A.I.
Survey of the flight efficiency of a long-haul aircraft under uncertainty of tasks
Markiewicz P.
Optimizing the process of changing spacecraft orbital parameters by using a spinning electrodynamic tether sytem
Lu H., Wang C., Zabolotnov Y.M.
Features of optimization of the versatile gas generator parameters and design for development of a broad power range line of the advanced gas turbine engines of different application
Sharova N.A.
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.
Analysis of the possibility of using topology optimization in the design of uncooled turbine rotor blades
Vasilyev B.E., Magerramova L.A.
Formation of a method of choosing rational values of ultralow power turbine parameters in a turbine drive system
Kalabuhov D.S., Grigoryev V.A., Rad’ko V.M.
Approaches to parametric models of blade machines formation
Shabliy L.S., Popov G.M., Kolmakova D.A.
Assessing the efficiency of flights to high near-earth orbits using boosters with chemical and electro-rocket engines
Ishkov S.A., Fadeenkov P.V., Balakin V.L.
Optimal distribution of turboprop engine free energy between the screw and the jet with mass characteristics taken into account
Grigoriev V.A., Prokaev A.S.
The rotation maneuvers and synthesis of gyromoment guidance laws for land-survey spacecraft
1 1., 1 1., 1 1.
Way of increase in efficiency of cycle gas turbine units
1 1.
Optimizing the propulsion of a hypersonic accelerator aircraft of a two-stage aerospace system
Balakin V.L., Bebyakov A.A., Kotchyan A.G.
Determination of the optimal parameters and engine layout for a strike unmanned aerial vehicle
Zinenkov Y.V., Lukovnikov A.V., Agaverdyev S.V.
Fuzzy-controller simulation model as a tool of optimization of a limited availability ground handling system at a hub airport
Romanenko V.A.
Optimization of fuel distribution in the afterburner of a gas turbine engine
Nelyubin V.R.
Development of the criteria of analyzing the stress-strain state of gas turbine engine parts in the elastoplastic range
Bukaty A.S., Bukaty S.A.
Optimization of the schedule of financing of the investment project on graphs of works for oil and transport branches
Morozova S.A.
Peculiarities of laser welding of thin parts of aerospace equipment
Smelov V.G., Sotov A.V., L’vov M.V.
Simulation of manufacturing processes within the concept of «lean production»
Smelov V.G., Kokareva V.V., Shitarev I.L.
Choice of design parameters of universal platforms of small space vehicles
Volotsuev V.V., Tkachenko I.S., Safronov S.L.
Aerodynamic improvement of GTE compressors by space profiling of blade vanes
Gerasimenko V.P., Shelkovsky M.Y.
Through optimization of branching trajectories in view of random disturbances
1 1., 1 1.
The optimization of the turbine blade-disk interlock of the type “fir tree”
1 1., 1 1.
Synthesis of combined methods of sun spectrometry method of continual spectral measurements
Godjayeva L.S.
Gasdynamic and strength improvement of the axial flow turbine of a helicopter gas turbine engine
Goriachkin E.S., Popov G.M., Matveev V.N., Shcherban A.I., Kudryashov I.A., Melnikov S.A.
Probability-based genetic algorithm for solving complex multiobjective optimization tasks using adaptive mutation operator and Pareto set prediction
Sopov Y.A., Sopov S.A.
Automated construction of a fan blade model according to data of CAD profile measurements
Arkhipov A.N., Bugrjashova E.V., Ravikovich Y.A., Savin R.A., Terentjev V.V., Shevjakov A.O.
Modeling in management systems
Krasnoschekov A.D., Tyulevin S.V., Kozlova I.A., Tokareva A.V.
Optimization model of financing production of an industrial enterprise of space-rocket industry
Inozemtsev V.V.
Problems of ultralow power turbine design in a turbine drive system
Kalabuhov D.S., Grigoryev V.A., Rad’ko V.M.
Gas turbine engine designing on the basis of a unified gas generator
Rybakov V.N.
High fidelity modeling at early stages of airframe structural design
Boldyrev A.V., Komarov V.A.
Improving the quality parameters of serial debug two spool mixed flow turbofan
Volik A.A., Gumerov K.S., Khabibullin R.Z., Khayrullin R.B.
Dynamic analysis and optimization of turbojet engine nozzle control mechanism
Statistical modeling of the process of serving the leaving passengers at the international Kurumotch airport
Romanenko V.A.
Forming the conceptual structure of a dimensionally stable platform by numerical optimization
Peresypkin K.V., Kozhichenkova M.S.
Optimizing the allocation of technological resources of an air transport system in the presence of a schedule and fuzzy input data
Romanenko V.A.
Vector optimization of the parameters of a queueing system with partial mutual assistance between channels
Romanenko V.A.
Topology optimization of a load-bearing structure via the method of convex linearization
Kishov E.A., Komarov V.A.
Simulation of wire manufacturing production cycle
Haymovich I.N., Skripachyov D.G., Kolesnikova S.Y.
Forecasting and optimization of supplies in case of demand fluctuations
Gorlach B.A., Saveliev G.L.
Economic-mathematical model of optimizing financial cycles of bearing industry enterprises
Geraskin M.I., Yegorova V.V.
Optimization features of the working process parameters of bypass engine on the basis of given gas generator
Rybakov V.N.
Fuzzy optimization of the passenger airlines network based on the hubs airports system
Romanenko V.A.
Symmetric airfoil shape optimization using the adjoint gradient method for viscous turbulent incompressible flow
Pechenik E.V.
Solving the problem of stabilizing program deployment of an orbital tether system taking into account limitations on the rotary motion of the tip body
1 1., 1 1.
Optimization of material distribution in load-bearing units for several cases of loading
Boldyrev A.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.
Methods of validation of the ballistic structure of space surveillance system orbital segment
Fadin I.A., Yanov S.V., Samokhvalov O.A.
Optimization of ducted counter–rotating fan blades on the basis of solving a 3d inverse problem with the aim of improving fan gasdynamic characteristics
Mileshin V.I., Pankov S.V., Fateyev V.A., Shchipin S.K.
Stochastic optimal integration of hub airport technological resources
Romanenko V.A.
Models and methods of corporation management in case of inter-corporation interaction
Geraskin M.I.
Models of discrete multycriterion optimization for hierarchical systems of corporations
Geraskin M.I.
Improving the high pressure compressor efficiency by optimizing the stator blades angles
Popov G.M.
Use of the dynamic programming method for solving tasks of GTE management optimization using the aircraft efficiency criteria
Tkachenko A.Y., Kuzmichev V.S.
Determination of mass-power propertions for parametric range of launch vehicle modifications
Baranov D.A., Yelenev V.D.
Assessing weight efficiency of carrier rockets launched from dirigibles and airplanes
Kurenkov V.I.
Designing of minimum mass airframes under several loadings
Danilin A.I.
Modeling of dynamics of system with relaxation hysteretic damping
Shakirov F.M.
Locally optimal control of space tug motion between the libration points of the Earth-Moon system
Starinova O.L., Fain M.K.
Comparative research of algorithms of measuring the geometry of complex profiles of gas turbine engine compressor blades
Pechenin V.A., Bolotov M.A., Ruzanov N.V., Stepanova E.R.
Method of parametric optimization of each component of adaptive compensatng inertial sensors operating in a self-oscilation mode
Fominov I.V.
Searching for optimal configuration of aircraft with annular wings
Lazarev A.Y., Semenov V.N.
Problem of multistage compressor optimization while designing perspective gas turbine engines
Shabliy L.S.
Optimization of aircraft seven stage compressor first stages parameters
Popov G.M., Matveev V.N., Baturin O.V., Kolmakova D.A.
Opntimization of business processes for design and technological planning of production using SADT technologies for the Samara metallurgical plant "ALCOA"
Zelenev A.V., Khaimovich I.N.
Designing GTE on the basis of versatile gas generator small dimension
1 1., 1 1.
Laser optico-acoustical octane meter in systems of optimizing the process of commercial petrol compound-filling
Astapov V.N.
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.
The development of the optimization methodology of the turbine blade-disk interlock of the type “fir tree”
Bukaty A.S., Bukaty S.A., Andreev I.B.
Mathematical model and optimization of helicopter vertical takeoff considering operational conditions and aerodynamic damping
Onushkin Y.P., Sizov D.A., Poluyakhtov V.A., Ostrovoy A.V.
The use of mathematical optimization means to increase the efficiency of a seven-stage axial flow compressor
Baturin O.V., Popov G.M., Gorachkin E.S., Novikova Y.D.
Improving the accuracy of assessing the position deviation in coordinate measurements of GTE compressor and turbine blade profiles
Bolotov M.A., Pechenin V.A., Ruzanov N.V.
Parametrical optimizing of a transfer air transportation system in conditions of uncertainty
Romanenko V.A.
Designing of the aviation engine's hydrodynamic bearing
Parovay Y.F., Gordeev V.B., Falaleev S.V.
Influence of the initial design data uncertainty on the choice of optimal working process parameters of gas turbine engine
Kuzmichev V.S., Tkachenko A.Y., Rybakov V.N., Krupenich I.N., Kulagin V.V.
Problems of mathematical programming in optimization of controlling air transportation on the basis of a hub airport
Potapov I.V., Romanenko V.A.
Optimization characteristics of rotor-support system from NK-14ST free power turbine with consider statics and dynamics propertys
1 1., 1 1.
Creation of the database for electrochemical processing with the purpose of optimization of process of the choice of electrolit
Smelov V.G., Shitarev I.L., Smirnov G.V.
Optimization of honeycomb sandwich floor panels made of polymer-matrix low-combustible composite materials based on high-strength carbon and glass fibers and adhesive binder
Komarov V.A., Kutsevich K.E., Pavlova S.A., Tyumeneva T.Y.
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.
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.
Optimization of the workflow of multistage axial turbines with platforms
Matveev V.N., Baturin O.V., Popov G.M., Goryachkin E.S.
Estimation of mass-dimensional characteristics of a complex propulsion unit of earth remote sensing spacecraft
Kurenkov V.I., Kucherov A.S., Yakishik A.A.
Experimental verification of the specified characteristics of a solar battery at the stages of production and ground operation
Shuplyak Y.P., Sorokoletov V.I.
Models of reliability and determination of acceptable periodicity of maintenance of ageing aircraft fleet
Pisarenko V.N.
Problem formulation of bypass engine parameters optimization with a preselected gas generator
Kuzmichev V.S., Kulagin V.V., Tkachenko A.Y., Krupenich I.N., Rybakov V.N.
Model and technique of optimization of the schedule of financing of investment projects
Morozova S.A.
Features of designing gas turbine of complex cycle GT24
1 1.
The using of computational modeling for design of gas turbine engines with decreased blowout nitrogen oxides
Gulina S.A., Orlov M.Y., Uglanov D.A.
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