Dynamic behaviour of high- bypass- ratio turbofan carbon fiber-reinforced plastic blade ubder unsteady airloads
Buyukli T.V., Fedorchenko Y.P., Shorstov V.A.
Methodical features of vibration tests of rotating blades using dynamic spin rigs
Nozhnitsky Y.A., Fedina Y.A., Shadrin D.V.
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.
Construction of a blade beam finite element as a component of the blade disk rotary-symmetrical system
Davydov D.P.
Design of the gas turbine engine rotor wheel with ceramic blades
Sapronov D.V., Reznik S.V.
Investigation of structural damping of turbomashine blade vibrations using dynamic spin rigs
Nozhnitskiy Y.A., Fedina Y.A., Shadrin D.V.
3D modeling of blade flutter in modern gas turbine engines
Vedeneev V.V., Kolotnikov M.E., Makarov P.V., Firsanov V.V.
Automatization of creation vane models for CAE with PROFILER
Shabliy L.S., Dmitrieva I.B., Popov G.M.
Experimental design of a device for bird strike bench tests of non-rotating fan blades
Shorr B.F., Matsarenko V.S., Serebryakov N.N.
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.
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.
Development of the construction of a gas turbine engine vane with built-in vortex tubes
Veretennikov S.V., Barinov S.N.
Development of automated software module for modelling of forming part of electrochemical GTE
Nekhoroshev M.V., Pronichev N.D.
The projecting of gas turbine engine composite blades
Ryzhov A.A., Galimkhanov B.K., Ryzhov N.A., Latypov R.K., Irgalin S.R.
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.
Investigation of thermal conditions nozzle blades with a cyclone-vortex cooling system
Veretennikov S.V., Khasanov S.M.
Analysis of the stressed state of high-speed extrusion process
Kostyshev V.A., Pityugov M.S.
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.
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.
Approaches to parametric models of blade machines formation
Shabliy L.S., Popov G.M., Kolmakova D.A.
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.
Compressor blade profile reverse-engineering: building of middle curve and symmetrical profile
Shabliy L.S.
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.
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.
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.
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.
The prowiding of the given fccuracy of the second tipe dimensions for finished pulse electrochemical machining of low stiffness detals
Smirnov G.V.
Hydrogenium saturation research for finishing pulsed electrochemical machining of titan alloy (BT9) TJ blades
Smirnov G.V.
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.
Ways 3D parametrization TJ blades for use CAD/CAM/CAE packages
Smelov V.G., Shitarev I.L.
Evaluation of turbine rotor blade life taking into account static and thermal cyclic loading
Badamshin I.K.
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.
Damping devices in the construction of compressor vanes of engines of the "NK" family
Frolov V.A., Belousov 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.
3D-model of compressor rotor blade development
Boyarov K.V., Ryazanov A.I., Chempinsky L.A.
Automatization of creation vane 3D-model in Ansys TurboGrid with geometry data in traditional view
Dmitrieva I.B., Shabliy L.S.
About relaxational resistance of the compressor’s blades from titanium alloys
Smyslov A.M., Smyslova M.K., Dubin A.I.
1 - 39 of 39 Items

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