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.
Construction of a blade beam finite element as a component of the blade disk rotary-symmetrical system
Davydov D.P.
Dynamic behaviour of high- bypass- ratio turbofan carbon fiber-reinforced plastic blade ubder unsteady airloads
Buyukli T.V., Fedorchenko Y.P., Shorstov V.A.
The projecting of gas turbine engine composite blades
Ryzhov A.A., Galimkhanov B.K., Ryzhov N.A., Latypov R.K., Irgalin S.R.
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.
Discrete-phase movement transducers for the determination of turbine blade vibration parameters
Danilin A.I., Grechishnikov V.M.
Effect of radial location of nozzles on width on performance of pre-swirl systems
Didenko R.A., Karelin D.V., Ievlev D.G., Lebedev V.V.
Design of the gas turbine engine rotor wheel with ceramic blades
Sapronov D.V., Reznik S.V.
Methods of the blade release at casings containment capability
Baluev B.A.
Calculated study of tangential inclination of nozzle vanes influence on gas-dynamic efficiency of axial turbine stage
Baturin O.V., Matveev V.N.
Fatigue resistange of turbine blade roots under combined stress
Gladkov A.V., Solyannikov V.A., Zhuzhukin A.I.
Technique of operational monitoring of blade operational life exhaustion on turbounits
Danilin A.I., Grechishnikov V.M.
3D modeling of blade flutter in modern gas turbine engines
Vedeneev V.V., Kolotnikov M.E., Makarov P.V., Firsanov V.V.
Experimental design of a device for bird strike bench tests of non-rotating fan blades
Shorr B.F., Matsarenko V.S., Serebryakov N.N.
Rotor blade compressor working process analysis
Dovgyallo A.I., Kolomin I.V.
Fast algorithm for finding the resonance frequencies of gas turbine engine rotating blade disks
Davydov D.P.
Methodological support for the training of UAV designers and operators
Lukyanov O.E., Zolotov D.V.
Calculation of exciting aerodynamic load on a gas turbine engine compressor blade induced by the effect of a non-uniform gas flow
Ermakov A.I., Shklovets A.O., Fedorchenko D.G.
Development of the construction of a gas turbine engine vane with built-in vortex tubes
Veretennikov S.V., Barinov S.N.
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 description of the interaction between a probing microwave signal and the helicopter main rotor blade
Danilin A.I., Zhukov S.V., Popov M.S.
Investigation of thermal conditions nozzle blades with a cyclone-vortex cooling system
Veretennikov S.V., Khasanov S.M.
Effect of cavity width on performance of pre-swirl systems
Didenko R.A., Karelin D.V., Ievlev D.G., Lebedev V.V., Belousova E.V.
Application of numerical simulation systems for the research of the blade casting process in blank production
Smelov V.G., Vdovin R.A., Agapovichev A.V.
GTE parts optimal design
Temis Y.M., Yakushev D.A.
Investigation of structural damping of turbomashine blade vibrations using dynamic spin rigs
Nozhnitskiy Y.A., Fedina Y.A., Shadrin D.V.
Reduction of circumferential variation in the final stage of IPC
Popov G.M., Mamedov A.C., Smirnova Y.D.
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.
About some directions in development avation engine buildings
Zamtfort B.S.
The devices for the diagnosis and control of turbine blades deformative condition during operation
Danilin A.I., Chernyavskiy A.G., Kapustin A.S.
Evaluation of turbine rotor blade life taking into account static and thermal cyclic loading
Badamshin I.K.
Automatization of creation vane models for CAE with PROFILER
Shabliy L.S., Dmitrieva I.B., Popov G.M.
Formation of film cooling on the turbine blade back and pressure side in the case of using V-shaped dimples
Lebedev V.V., Lebedev O.V., Remizov A.E.
Parameters transducers of the blade’s dynamic movements of turbounits based on nonlinear approximation of primary signals
Chernyavskiy A.Z., Danilin A.I., Danilin S.A.
Reduction of circumferential variation in the final stage of IPC
Baturin O.V., Krivcov A.V., Matveev V.N., Popov G.M.
Improvement of fretting wear resistance of blade root made of polymer composite material
Karimbayev T.D., Afanasiev D.V., Matyukhin D.V., Orlov M.A.
Thermoplastic strengsening of blades aircraft gas turbine engines
Krotinov N.B.
The prowiding of the given fccuracy of the second tipe dimensions for finished pulse electrochemical machining of low stiffness detals
Smirnov G.V.
The device for the determination of blades oscillation parameters based on nonlinear approximation of primary transducers signals
Danilin A.I., Chernyavskiy A.Z., Danilin S.A.
Research of the mechanism of shock-inertial deposition of dispersed particles from a gas flow
Usmanova R.R., Zhernakov V.S.
Hydrogenium saturation research for finishing pulsed electrochemical machining of titan alloy (BT9) TJ blades
Smirnov G.V.
Analysis of the stressed state of high-speed extrusion process
Kostyshev V.A., Pityugov M.S.
Study of uncertainty of measuring geometrical parameters of gas turbine engine compressor blade profiles
Pechenin V.A., Bolotov M.V., Ruzanov N.V., Yanyukina M.V.
Approaches to parametric models of blade machines formation
Shabliy L.S., Popov G.M., Kolmakova D.A.
Ways 3D parametrization TJ blades for use CAD/CAM/CAE packages
Smelov V.G., Shitarev I.L.
Compressor blade profile reverse-engineering: building of middle curve and symmetrical profile
Shabliy L.S.
Theoretical basis of forming forging impellers of blade machines in multichannel stamps
Vorobjev V.M.
Mathematical model of complex spatial deformation of rotor blades during helicopter arbitrary motion
Girfanov A.M.
Research of the process of cleaning gas from mechanical impurities in a direct flow centrifugal separator
Glebov G.A., Hazbulatov A.I.
Automated system for measuring geometric parameters of turbine blades in production conditions
Aleksentsev E.I., Shavrin P.A., Fedoseev O.B.
Fan engine research
Murzagaliev A.G., Nekrasov V.G.
Perfection of technological preparation of manufacture of blades of compressor GTD on the basis of use of parametrical models
Orlov R.R., Pronichev N.D., Chempinsky L.A.
Damping devices in the construction of compressor vanes of engines of the "NK" family
Frolov V.A., Belousov A.I.
3D-model of compressor rotor blade development
Boyarov K.V., Ryazanov A.I., Chempinsky L.A.
Calculation and experimental investigations on the efficiency of various ways of vibration damping of jet engine parts
Shorr B.F., Serebryakov N.N., Stadnikov A.N., Shadrin D.C., Rudenok E.S., Kanackin A.V., Bortnikov A.D.
About relaxational resistance of the compressor’s blades from titanium alloys
Smyslov A.M., Smyslova M.K., Dubin A.I.
Experimental determination of thermal-fatigue life of turbine blades with various coatings made of an advanced heat resistant nickel alloy
Bychkov N.G., Nozhnitsky Y.A., Khamidullin A.S., Pershin A.V., Avrutsky V.V.
Probabilistic estimate of compressor blades durability to foreign object damage
1 1., 1 1.
Research of the postoperational condition of the restored compressor shovels of GTD gas-transfer of the units which have fulfilled the appointed resource
Tarasenko Y.P., Tsareva I.N., Krivina L.A.
Blading of radial-axial turbine wheel using Bezier curve
Baturin O.V.
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