Method of calculating GTE gas-thermodynamic parameters with blade row description of an axial multistage compressor
Boyko L.G., Karpenko E.L., Akhtemenko U.F.
Method of lossless image compression in the Earth remote sensing systems
Petrov E.P., Kharina N.L., Sukhikh P.N.
The influence of the shuttle effect on the intensification of heat losses in a Stirling engine
Savchenko V.A., Stolyarov S.P.
Theoretical and experimental analysis of the thermal state of transport aircraft compartments thermal state
Nikolayev V.N.
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.
Calculation method for determining the characteristics of elastic-damping suspension made of metal analoque of rubber for plain bearings
Parovay Y.F., Parovay F.V.
Heat exchange parameters of units and pipelines of the aircraft hydraulic system
Nikolayev V.N.
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.
Research of small spacecraft dynamiсs taking into account the influence of elastic vibrations of asjacent solar panels and aerodynamic moment
Yelenev V.D., Titov B.A., Davydov E.I., Davydov I.E., Kochyan A.G., Yudintsev V.V.
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.
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.
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.
Method of reducing design aerodynamic characteristics to the results of drain tests of a transport category aircraft model
Bondar Y.I.
Assessing reduction gear mass in the problem of optimizing parameters of the working process of a turboprop engine at the initial design stage
Grigoryev V.A., Zagrebelnyi A.O., Prokaev A.S., Kuznetsov S.P.
Dynamic process modeling of aircraft engine control system
Blyumin K.V.
ASMTurbC method of autonomous statistical modeling of diffusion turbulent combustion and the results of its testing
Nuzhnov Y.V.
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.
Real-time control algorithms requirements verification mathematical model implementation in visual design computer-aided system
Shulyndin A.V., Tjugashev A.A.
Hemispherical high-speed particle transducer
Izyumov M.V., Syomkin N.D.
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.
Universal approach to the description of working medium chambers for simulating hydraulic and pneumatic systems
Timofeyev Y.M., Khalatov E.M.
Coordination of process management mechanisms for design and technological planning of production at the level of staff members
Kirichenko A.S., Khaimovich I.N.
Mathematical model of training and self-training in maintenance of complicated systems
Koptev A.N., Popovich A.A.
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.
A hot-wire anemometric transducer of airflow mass rate
Nikolayev V.N.
Development of discrete pneumatic pressure regulator and researching of its characteristics
Greshniakov P.I., Sinyakov A.F., Ilukhin V.N.
Research of the process of sheet presswork using polyurethane under constrained bending
Eskina E.V., Gromova E.G.
The development of mathematical models of acoustic characteristics of the elastic porous material «metal-rubber»
Safin A.I., Igolkin A.A.
Laser optico-acoustical octane meter in systems of optimizing the process of commercial petrol compound-filling
Astapov V.N.
Study of characteristics of the launch vehicle fuel line gas damper
Gimadiev A.G., Odinokov D.A., Stadnik D.M., Greshnyakov P.I.
Optimization of model positional harakterstik of the electromagnetic sensor of the linear peremeshchny
Tingaev V.S., Matyunin S.A., Mednikov V.A.
Analysis of on-board equipment robustness on the basis of COTS-products
Yefanov V.N., Bondarev A.V.
Calculation methodology of intermittent burning chamber main parameters
Solodovnikov A.V., Vishegorodcev E.N., Golubyatnik V.V.
Simulation of automatic systems of controlling space vehicle drives
Zhuravlyova Y.V.
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.
Model of varigrained particle stream moving by hypersonic combustion materials investigation
Bulanova E.A., Pervishin A.N.
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.
Dynamic of the a safety vent valve
Makaryjants M.V., Kudyurov L.V., Mustafaev Y.K., Tumanov D.V.
Plane high-speed particle transducer
Izyumov M.V., Syomkin N.D.
Computer-aided system of virtual gas turbine engine testing
Tkachenko A.Y., Rybakov V.N., Krupenich I.N., Ostapuk Y.A., Filinov E.P.
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.
Mathematical model and peculiarities of operating mobile robots with hybrid drives
Ilyukhin Y.V., Tatarintseva A.V.
Simulation and research of factors affecting aerodynamic indices of the gas purification process
Usmanova R.R., Zhernakov V.S.
Simulator, algorithm and software for the computation of differential gas circuits frequency response
Igonin A.A., Gimadiev A.G.
Constructing the specification for the on-board realtime control algorithm
Tyugashev A.A., Bogatov A.Y.
Mathematical modeling of heat exchange on air cooling of a number of aluminum ingots
Gorshenin A.S.
Mathematical model of anisotropic elastic-plastic material
Grechnikov F.V., Yerisov Y.A.
Simulation of aerodynamic structure of the flow in the combustion chamber of a small-size gas turbine engine with the help of CAE–systems
Matveev S.G., Orlov M.Y., Abrashkin V.Y., Zubrilin I.A., Matveev S.S.
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.
Simulation of the distributed selection and supply of cooling air in gas-turb engine
Goryunov A.I., Goryunov I.M.
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.
Set-theory model of the aircraft hydraulic system working fluid state
Koptev A.N., Gareyev A.M., Popelnyuk I.A.
System-mathematical simulation of engine air hydraulic power supply
Goryunova N.R., Goryunov A.A.
Increase of stability of technological systems at processing of details aircrafts engines
Skuratov D.L., Burmistrov E.V., Samykin V.N.
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.
Micro gas turbine engine imitation model
Kuznetsov A.V., Makaryants G.M.
Control over the deployment of an orbital tether system of great length
Wang C., Zabolotnov Y.M.
Mathematical model of an eddy current converter for testing discontinuous structure samples
1 1., 1 1.
Non-linear image filtration based on Markovian networks with several states
Petrov Y.P., Kharina N.L., Rzhanikova Y.D.
Mathematical models of squeeze film dampers in rotor dynamics of gas turbine engines
Kutakov M.N., Degtiarev S.A., Leontiev M.K.
Parameters study in the electrothermal and jet protection of the airliner cockpit windows from fogging
Nikolayev V.N.
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.
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.
Analysis of the cause of serious flight accident
Vakhrushev D.E., Agaphonov O.A., Pryadko S.P., Schukin A.V.
Frequency characteristics of a coaxial gas damper for booster feed line
Odinokov D.A., Gimadiyev A.G.
Experimental and theoretical research of continuous motion of rotor on anisotropic gapped elastic support
Nikiforov A.N., Panovko G.Y., Shokhin A.Y.
Mathematical model of surface layer formation during hydroabrasive jet machining
Meshcheryakov A.V., Shulepov A.P.
Control program for noncoplanar heliocentric flight to Venus of non-perfectly reflecting solar sail spacecraft
Khabibullin R.M.
Process of coating the inner surface of an inclined pipe and its mathematical modeling
Skvortsov B.V., Zaretskaya M.I., Zaretskiy I.S., Zhivonosnovskiy P.A.
Simulating of Roots compressor
Belov G.O., Ermilov M.A., Kryuchkov A.N.
Оptimization of gas turbine aircraft engine control throughout the engine service life
Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.
Using the «virtual engine» software in automatic control system of gas turbine engine
Golberg F.D., Gurevich O.S., Petukhov A.A.
Double-electrode electrochemical cell volumetric and flat simulation using ANSYS program
Nekhoroshev M.V., Pronichev N.D., Smirnov G.V.
Transducer of fluid and air consumption and temperature in pipelines
Nikolayev V.N., Kabanov Y.N.
Design build process for the accuracy of eligibility
Grechnikov F.V., Tlustenko S.F.
Concept of construction of virtual lab for gas turbine engine testing
Rybakov V.N., Kuzmichev V.S., Tkachenko A.Y.
Mathematical modeling of a controlled electromechanical actuator for special assembly and coupling equipment
Nosov A.S.
Dataware of virtual lab for gas turbine engine testing
Rybakov V.N., Kuzmichev V.S., Kulagin V.V., Krupenich I.N., Fedorov D.V.
Quality forecasting solder joint electronic components
Shumskikh I.Y.
The concept of generalized method of calculation and design of wet cleaning duct GTD
Silaev B.M., Malcev E.N.
Mathematical modeling of technological production process of thermo-stable resistor – capacity structures
Merkulov A.I., Laktanov P.V., Merkulov V.A.
Dynamik experimental researches of the face gas dynamic seal
Novikov D.K., Balyakin V.B., Sedov V.V.
Mathematical modeling of interaction a high-frequency torch discharge with construction elements of radio equipment
Kostin A.V., Piganov M.N., Stolbikov A.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.
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.
Mathematical model of mastering educational information of the academic process
Titov B.A., Ryabinova E.N.
Approximation of characteristics of linear displacement inductive sensors using modified Gaussian function with a first order difference argument
Tingaev V.S., Matyunin S.A., Mednikov V.A.
The development of mathematical model of hydrodynamics of "tpapped" volume in the gear pump
1 1., 1 1., 1 1., 1 1., 1 1.
Mathematical models for evaluating the energy efficiency of ultralow power turbine drives
Kalabuhov D.S., Grigoryev V.A., Rad’ko V.M.
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.
Theoretical and experimental investigation of the photographic reconnaissance plane instrument bay thermal state
Nikolayev V.N.
Research of hydrodynamic processes in the lubrication system of gas turbine engines
Gulienko A.I., Shchurovskiy Y.M.
Mathematical model of small-thrust rocket engine with gaseous oxygen and hydrogen in pulse operation
1 1.
Improving the operating characteristics of engines by the imposition of manufacturing operation of hermeticity inspection of vacuum-tight radio electronic device cases
1 - 95 of 95 Items

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