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Title
Authors
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.
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.
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.
Calculated study of tangential inclination of nozzle vanes influence on gas-dynamic efficiency of axial turbine stage
Baturin O.V., Matveev V.N.
Evaluation of turbine rotor blade life taking into account static and thermal cyclic loading
Badamshin I.K.
Development of the construction of a gas turbine engine vane with built-in vortex tubes
Veretennikov S.V., Barinov S.N.
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.
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.
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.
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.
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.
Thermoplastic strengsening of blades aircraft gas turbine engines
Krotinov N.B.
Approaches to parametric models of blade machines formation
Shabliy L.S., Popov G.M., Kolmakova D.A.
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.
Probabilistic estimate of compressor blades durability to foreign object damage
1 1., 1 1.
Automated system for measuring geometric parameters of turbine blades in production conditions
Aleksentsev E.I., Shavrin P.A., Fedoseev O.B.
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.
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.
1 - 20 of 20 Items

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