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Determining aerodynamic characteristics of small unmanned aerial vehicles involving flight experiment
Lukyanov O.E., Zolotov D.V., Espinosa Barsenas O., Komarov V.A.
Experimental and analytical determination of the elastic characteristics of layered woven composites
Komarov V.A., Pavlov A.A., Pavlova S.A.
Influence of pad geometry and method of oil supply on the thermal state of GTE rotor tilting-pad journal bearing
Parovay E.F.
Some questions of designing and manufacture of wire material hub dampfers
Lazutkin G.V., Parovay F.V., Troynikov A.A.
Elastic damping and dynamic characteristics of vibration isolators made of wire materials of different types
Yermakov A.I., Lazutkin G.V., Parovay F.V., Boyarov K.V., Bondarchuk P.V., Davydov D.P.
Measuring system for investigation flow rate and fluid pressure features of control devices for the position hydrodrive
Poleshkin M.S., Sidorenko V.S.
Procedure of accomodation of earth remote sansing satellite external devices with regard for the satellite target operation
Akhmetov R.N., Shilov L.B., Kurenkov V.I., Yakischik A.A.
Calculation of vibroacoustic characteristics of a four-point ball bearing. Part 2
Kurushin M.I., Kurushin A.M., Zhilnikov Y.P., Murashkin V.V.
Imitation models of aircraft hydraulic units with account for typical faults
Gareyev A.M., Popelnyuk I.A., Stadnik D.M.
Peculiarities of the working process of low-thrust hypergolic-propellant liquid rocket engines with a thrust of less than 1 N
Nigodjuk V.E., Sulinov A.V.
Study of characteristics of the launch vehicle fuel line gas damper
Gimadiev A.G., Odinokov D.A., Stadnik D.M., Greshnyakov P.I.
Method of choosing spacecraft design characteristics on the basis of creating task-oriented systems of computer-aided design
Kucherov A.S., Kurenkov V.I.
Design and research of characteristics of a pressure fluctuation damping device for electrocontact manometers
Gimadiev A.G., Gimadiev A.A., Ermochkin A.Z., Ilyuchin V.N.
Modeling static and dynamic characteristics of pressure reducing valves
Igolkin A.A.
Rotor blade compressor working process analysis
Dovgyallo A.I., Kolomin I.V.
Homogeneous burners of two-staged combustion chambers
Grechishnikov O.V., Ostapets I.I., Roslyakov A.D., Tsybizov Y.I.
Calculation of vibroacoustic characteristics of a four-point ball bearing. Part 1
Kurushin M.I., Kurushin A.M., Zhilnikov Y.P., Murashkin V.V.
Engines for domestic drones: past, present and future
Cherkasov A.N., Legkonogikh D.S., Zinenkov Y.V., Panov S.Y.
Procedure of designing a pilot operated gas pressure regulator for launch vehicle fuel tanks
Gimadiev A.G., Sverbilov V.Y., Stadnik D.M.
Calculation of sleeve-shaped filter elements made of the MR material
Zhizhkin A.M., Lazutkin G.V., Volkova T.V.
Improving the high pressure compressor efficiency by optimizing the stator blades angles
Popov G.M.
Optimization of aircraft seven stage compressor first stages parameters
Popov G.M., Matveev V.N., Baturin O.V., Kolmakova D.A.
Construction of a blade beam finite element as a component of the blade disk rotary-symmetrical system
Davydov D.P.
Development of the finite element model of vibroacoustical characteristics of pipe system
Mironova T.B., Prokofiev A.B., Shahmatov E.V.
Thermal state of a groind-use gas turbine engine stator
Grechishnikov O.V., Balakin A.Y., Roslyakov A.D.
Design and development of combustion chambers for gas turbine engines based on calculations of various levels of complexity
Aleksandrov Y.B., Nguyen T.D., Mingazov B.G.
Optimization of open counter – rotation fan blades on the basis of solving a 3D Navier-Stokes inverse problem with the aim of reducing tonal noise
Mileshin V.I., Rossikhin A.A., Pankov S.V., Shchipin S.K.
Procedure of comparative assessment of the efficiency of Earth remote sensing satellites with different optoelectronic telescopic complexes
Stratilatova N.N., Kurenkov V.I., Kucherov A.S., Egorov A.S.
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.
Development of discrete pneumatic pressure regulator and researching of its characteristics
Greshniakov P.I., Sinyakov A.F., Ilukhin V.N.
Investigation of effects of multistage compressor final stage blading shape on compressor performance and flow pattern
Popov G.M., Krivcov A.V., Kolmakova D.A.
Forming of the structure and properties of titanium alloys according to mechanical properties in the processes of plastic working of metals
Tlustenko S.F., Pervyshin A.N.
A method for estimating morphological parameters of vessels in fundus images based on curve visibility matrix
Ananyin M.A., Ilyasova N.Y.
Spacecraft preset orbital parameters control by means of thrusters
Salmin V.V., Volotsuev V.V., Shikhanov S.V.
Analysis of contact interaction of polymer honeycomb core and CFRP base layers in sandwich-core constructions
Pavlova S.A.
Efficiency of technical workings out in batch production GTE
Aleksentsev E.I., Shitarev I.L., Kurbatov V.P., Gritsenko E.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.
Experimental investigation of the efficiency of laserelectronic systems for aircraft surface remote sounding
Sazonnikova N.A.
Emission characteristics and temperature non-uniformity at the outlet of the gas turbine engine combustion chamber
Sabirzyanov A.N., Yavkin V.B., Alexandrov Y.B., Markushin A.N., Baklanov A.V.
The design shape and basic performances of small satellite of SSAU and SRP SRC “TSSKB-Progress”
1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1.
Computer-aided-design system for calculating adsorption thermodynamic characteristics
Zelenko L.S., Varfolomeyeva V.V., Kuznetsov V.Y., Fed’kayev A.V., Terentyev A.V., Buryak A.K.
System of satellite navigation of «Bion-M» space vehicle
Manturov A.I., Rublyov V.I., Muntyan R.Y.
Development of improved performance electromagnetic valve for liquid rocket engine
Igolkin A.A., Chubenko T.A., Maksimov A.D.
Investigation of laser beam influence on aircrafts surface condition estimation efficiency
Sazonnikova N.A.
Investigation of hydraulic and vibroacoustic characteristics of a prospective valve with an elastic tubular element used as the working body
Kryuchkov A.N., Romashov N.N., Ermilov M.A., Balyaba M.V.
Research of aperture characteristics of small length optical fibers
Paranin V.D., Dashkov M.V.
Dynamic elastic and damping models development and research for technical objects vibration safety providing
Shakirov F.M.
Laser measurement systems effectivity improvement for aircrafts and engines surface estimation
Sazonnikova N.A.
Influence of energy separation and vortex tube geometry on the flow turbulence
Piralishvili S.A.
Programme realization of mathematical operations of flow multiplexing and demultiplexing for network models
Bakhareva N.F.
Automated restoration of gas turbine engine characteristics by experimental data
Botchkaryov S.K., Mosoulin V.V.
Determination of the maximum values of the spatial angle of attack of a nanosatellite in motion on lowcircular orbits
Glukhova L.V., Timbai I.A.
Method for optimizing mass and size characteristics of a high-pressure turbine disk
Siluyanova M.V., Grunin A.N., Alendar A.D., Kandaurov S.K.
Working out of the design of the chamber of combustion of engine NK-14ST-10 with modular torches
Kocherov E.P., Rosljakov A.D., Tsibizov J.I.
The use of gas-dynamic flame stabilization in afterburner combustion chambers of aircraft gas turbine engines
Kolesnikov A.S., Pakhol'chenko A.A.
Thermal medical software hardware-based thermal imager COX CX - 320U
Davydov I.E., Agafonov A.N.
About some directions in development avation engine buildings
Zamtfort B.S.
Thermal state of combustor can elements
Grechishnikov O.V., Ostapets I.I., Roslyakov A.D., Tsybizov Y.I.
The detecting improvement by laser surface sounding
1 1.
Test rig for a hydraulic drive under switched inertance control
Shorin V.P., Sverbilov V.Y., Gimadiev A.G., Greshniakov P.I., Ilyukhin V.N., Stadnik D.M.
Determining the rheological properties of viscoelastic materials by the values of creep strain
Ivanov E.Y., Kirpichev V.A.
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.
Frequency characteristics of a coaxial gas damper for booster feed line
Odinokov D.A., Gimadiyev A.G.
Requirements for the order and the procedure of estimating structural strength characteristics of metal alloys for the main and critical parts of aviation gas turbine engines
Nozhnitsky Y.A., Kachanov E.B., Golubovskiy E.R., Kouevda V.K.
Matrix format of management interactions in the organization of enterprise development
Osmankin N.N.
Simulation modeling of stock markets
Steryakov A.A.
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 calculating of the load characteristics of cylindrical support with a discrete location of elastic damping elements of the MR material
1 1., 1 1., 1 1., 1 1., 1 1.
Chemical gas sources
Novikov A.A., Ershikhin N.A.
Determination of the optimal parameters and engine layout for a strike unmanned aerial vehicle
Zinenkov Y.V., Lukovnikov A.V., Agaverdyev S.V.
Life of gas turbine engine components under corrosive exposure
Pivovarova M.V., Gladkiy I.L.
Development of blend composition of aviation kerosene surrogate for the simulation of workflow of gas turbine engine combustion chamber
Matveev S.G.
Curcuit-design solutions for producing devices of feed water flow rate control systems
Berestovitsky E.G., Gladilin Y.A., Pyalov N.V., Solovyev M.V., Ermilov M.A.
Research of toxic substances emission during water injection into a combustion chamber
Mingazov B.G., Mukhametgaliev T.H.
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.
Finite element techniques for pipe system vibroacoustical characteristics modelling
Mironova T.B., Prokofiev A.B., Shorin V.P.
Wear resistance of chromium coatings, formed in trivalent electrolytes at presence of nanosized particles of metal oxides
Salakhova R.K., Semionychev V.V.
Features of the new gas turbine aviation engines theory course
Mingazov B.G., Kosterin V.A., Varsegov V.L.
Method of pipeline system designing taking into account complex interaction of static and dynamic processes with strength characteristics
Mironova T.B., Prokofiev A.B., Rodionov L.V.
1 - 79 of 79 Items

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