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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 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)

Vol 22, No 4 (2023)

Method of scanning thin surfaces in repairing gas turbine blades

Kotlyar D.I., Lomanov A.N.

(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)

Vol 7, No 3 (2008): Special Issue

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 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)

Vol 17, No 3 (2018)

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

Badamshin I.K.

(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)

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 14, No 3-1 (2015): Special Issue

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

Thermoplastic strengsening of blades aircraft gas turbine engines

Krotinov N.B.

(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 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 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 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)

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 3-3 (2012): Special Issue

Approaches to parametric models of blade machines formation

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

(Rus)

Vol 10, No 3-1 (2011): Special Issue

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 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 10, No 3-1 (2011): Special Issue

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

Probabilistic estimate of compressor blades durability to foreign object damage

1 1., 1 1.

(Rus)

1 - 23 of 23 Items

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