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Dynamic behaviour of high- bypass- ratio turbofan carbon fiber-reinforced plastic blade ubder unsteady airloads

Buyukli T.V., Fedorchenko Y.P., Shorstov V.A.

(Rus)

Vol 22, No 1 (2023)

Prospects of improving control over the process of electrochemical machining of the blade airfoil profile using the duplex mode method

Smirnov G.V., Shulepov A.P., Mescheryakov A.V.

(Rus)

Vol 22, No 1 (2023)

Verification of a transonic stage CFD model for assessing the erosion wear influence on the operation of the axial compressor

Blinov V.L., Zubkov I.S.

(Rus)

Vol 10, No 2 (2011)

Construction of a blade beam finite element as a component of the blade disk rotary-symmetrical system

Davydov D.P.

(Rus)

The projecting of gas turbine engine composite blades

Ryzhov A.A., Galimkhanov B.K., Ryzhov N.A., Latypov R.K., Irgalin S.R.

(Rus)

Methods of the blade release at casings containment capability

Baluev B.A.

(Rus)

Vol 20, No 4 (2021)

Special aspects of numerical simulation of a two-stage axial-flow compressor with defective blades

Blinov V.L., Zubkov I.S., Iskortsev E.Y., Belyaev O.V., Plishkin P.I.

(Rus)

Calculated study of tangential inclination of nozzle vanes influence on gas-dynamic efficiency of axial turbine stage

Baturin O.V., Matveev V.N.

(Rus)

Vol 22, No 4 (2023)

Method of scanning thin surfaces in repairing gas turbine blades

Kotlyar D.I., Lomanov A.N.

(Rus)

Vol 21, No 1 (2022)

The nature of change in the residual stress-strain state of dovetail lock joints, taking into account nonlinear strains

Zhernakov V.S., Mardimasova T.N., Koneva K.V.

(Rus)

Vol 10, No 3-3 (2011): Special Issue

Damping devices in the construction of compressor vanes of engines of the "NK" family

Frolov V.A., Belousov A.I.

(Rus)

Vol 16, No 3 (2017)

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.

(Rus)

Vol 10, No 5 (2011)

Research of the process of cleaning gas from mechanical impurities in a direct flow centrifugal separator

Glebov G.A., Hazbulatov A.I.

(Rus)

Vol 11, No 3-3 (2012): Special Issue

Approaches to parametric models of blade machines formation

Shabliy L.S., Popov G.M., Kolmakova D.A.

(Rus)

Vol 12, No 3-2 (2013): Vestnik SSAU

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.

(Rus)

The devices for the diagnosis and control of turbine blades deformative condition during operation

Danilin A.I., Chernyavskiy A.G., Kapustin A.S.

(Rus)

Vol 21, No 1 (2022)

Reconstruction of fan blade dynamic loading prior to its fracture

Artamonov M.A., Govorov A.A., Starshinov D.S.

(Rus)

Vol 10, No 3-3 (2011): Special Issue

3D-model of compressor rotor blade development

Boyarov K.V., Ryazanov A.I., Chempinsky L.A.

(Rus)

Vol 15, No 3 (2016)

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.

(Rus)

Vol 13, No 5-4 (2014): Special Issue

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.

(Rus)

Vol 11, No 3-2 (2012): Special Issue

Compressor blade profile reverse-engineering: building of middle curve and symmetrical profile

Shabliy L.S.

(Rus)

Vol 10, No 2 (2011)

Fast algorithm for finding the resonance frequencies of gas turbine engine rotating blade disks

Davydov D.P.

(Rus)

Vol 10, No 3-3 (2011): Special Issue

Blading of radial-axial turbine wheel using Bezier curve

Baturin O.V.

(Rus)

Vol 15, No 2 (2016)

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.

(Rus)

Vol 13, No 5-4 (2014): Special Issue

Development of the construction of a gas turbine engine vane with built-in vortex tubes

Veretennikov S.V., Barinov S.N.

(Rus)

Theoretical basis of forming forging impellers of blade machines in multichannel stamps

Vorobjev V.M.

(Rus)

Investigation of thermal conditions nozzle blades with a cyclone-vortex cooling system

Veretennikov S.V., Khasanov S.M.

(Rus)

Vol 10, No 1 (2011)

Technique of operational monitoring of blade operational life exhaustion on turbounits

Danilin A.I., Grechishnikov V.M.

(Rus)

Vol 20, No 1 (2021)

Methodological support for the training of UAV designers and operators

Lukyanov O.E., Zolotov D.V.

(Rus)

Vol 10, No 3-2 (2011): Special Issue

About relaxational resistance of the compressor’s blades from titanium alloys

Smyslov A.M., Smyslova M.K., Dubin A.I.

(Rus)

Vol 14, No 3-2 (2015): Special Issue

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.

(Rus)

Vol 13, No 5-1 (2014): Special Issue

Design of the gas turbine engine rotor wheel with ceramic blades

Sapronov D.V., Reznik S.V.

(Rus)

Investigation of structural damping of turbomashine blade vibrations using dynamic spin rigs

Nozhnitskiy Y.A., Fedina Y.A., Shadrin D.V.

(Rus)

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.

(Rus)

Vol 10, No 1 (2011)

Discrete-phase movement transducers for the determination of turbine blade vibration parameters

Danilin A.I., Grechishnikov V.M.

(Rus)

The prowiding of the given fccuracy of the second tipe dimensions for finished pulse electrochemical machining of low stiffness detals

Smirnov G.V.

(Rus)

Vol 18, No 4 (2019)

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.

(Rus)

Vol 10, No 3-2 (2011): Special Issue

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.

(Rus)

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.

(Rus)

Vol 11, No 7 (2012)

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.

(Rus)

Reduction of circumferential variation in the final stage of IPC

Popov G.M., Mamedov A.C., Smirnova Y.D.

(Rus)

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.

(Rus)

Vol 10, No 1 (2011)

Fatigue resistange of turbine blade roots under combined stress

Gladkov A.V., Solyannikov V.A., Zhuzhukin A.I.

(Rus)

Hydrogenium saturation research for finishing pulsed electrochemical machining of titan alloy (BT9) TJ blades

Smirnov G.V.

(Rus)

Vol 18, No 4 (2019)

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.

(Rus)

Vol 17, No 4 (2018)

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.

(Rus)

Vol 11, No 5-2 (2012): Special Issue

Thermoplastic strengsening of blades aircraft gas turbine engines

Krotinov N.B.

(Rus)

About some directions in development avation engine buildings

Zamtfort B.S.

(Rus)

GTE parts optimal design

Temis Y.M., Yakushev D.A.

(Rus)

Vol 8, No 4 (2009)

Mathematical model of complex spatial deformation of rotor blades during helicopter arbitrary motion

Girfanov A.M.

(Rus)

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.

(Rus)

Vol 10, No 3-4 (2011): Special Issue

Automated system for measuring geometric parameters of turbine blades in production conditions

Aleksentsev E.I., Shavrin P.A., Fedoseev O.B.

(Rus)

Vol 17, No 3 (2018)

Evaluation of turbine rotor blade life taking into account static and thermal cyclic loading

Badamshin I.K.

(Rus)

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.

(Rus)

Vol 11, No 5-2 (2012): Special Issue

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.

(Rus)

Vol 11, No 5-1 (2012): Special Issue

Automatization of creation vane models for CAE with PROFILER

Shabliy L.S., Dmitrieva I.B., Popov G.M.

(Rus)

3D modeling of blade flutter in modern gas turbine engines

Vedeneev V.V., Kolotnikov M.E., Makarov P.V., Firsanov V.V.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

Probabilistic estimate of compressor blades durability to foreign object damage

1 1., 1 1.

(Rus)

Ways 3D parametrization TJ blades for use CAD/CAM/CAE packages

Smelov V.G., Shitarev I.L.

(Rus)

Vol 10, No 3-4 (2011): Special Issue

Fan engine research

Murzagaliev A.G., Nekrasov V.G.

(Rus)

Vol 17, No 1 (2018)

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.

(Rus)