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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 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 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 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)

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

3D-model of compressor rotor blade development

Boyarov K.V., Ryazanov A.I., Chempinsky 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 5-2 (2012): Special Issue

Development of automated software module for modelling of forming part of electrochemical GTE

Nekhoroshev M.V., Pronichev N.D.

(Rus)

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

Veretennikov S.V., Khasanov S.M.

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

Automatization of creation vane 3D-model in Ansys TurboGrid with geometry data in traditional view

Dmitrieva I.B., Shabliy L.S.

(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)

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)

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 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)

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 4 (2012)

Analysis of the stressed state of high-speed extrusion process

Kostyshev V.A., Pityugov M.S.

(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)

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

Smirnov G.V.

(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)

Experimental design of a device for bird strike bench tests of non-rotating fan blades

Shorr B.F., Matsarenko V.S., Serebryakov N.N.

(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)

GTE parts optimal design

Temis Y.M., Yakushev D.A.

(Rus)

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

Smelov V.G., Shitarev I.L.

(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 17, No 3 (2018)

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

Badamshin I.K.

(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)

3D modeling of blade flutter in modern gas turbine engines

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

Vol 11, No 3-1 (2012): Special Issue

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

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

(Rus)