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Optimization of the Stage Number and Parameter Distribution in the Flow Passage at GTE Compressor and Turbine Design
Krivosheev I.A., Rozhkov K.E., Simonov N.B.
3D Investigations of the High Pressure Turbine Vane Platform Convection Cooling and Convection-Film Cooling
Gorelov Y.G., Anan’ev V.V.
Concept of monitoring for thermostressed state and service life of aircraft gas turbine engine blades
Kulikov G.G., Trushin V.A., Abdulnagimov A.I., Ganeev A.A.
Concepts of Gas Turbine Engine Improvement Through the Use of Choked-Flow Turbines
Bogdanov V.I.
Micro Gas Turbine Engine for Unmanned Aerial Vehicles
Sychenkov V.A., Limanskii A.S., Yousef W.M., Ankudimov V.V., Seyid Jafari S.S.
Research and Development of the Joint Seals for Gas Turbine Engine High-Temperature Turbine Stator Units
Belousov A.I., Borisov V.A., Parovai F.V.
3D Investigation of Film Cooling Effectiveness for Nozzle Vane Platform of High Pressure Turbine with “Meridian Constriction” and Laidback Fan-Shaped Film-Cooling Holes
Gorelov Y.G.
Integration of a High-Pressure Gas Turbine of the Gas Turbine Engine with a Gas-Dynamic Laser
Perel’shtein B.K., Osipov B.M., Titov A.V.
Study of performance of the aircraft gas turbine engine integrated with a gas dynamic laser
Osipov B.M., Kopelevich L.A., Perel’shtein B.K.
Radial two-stage microturbine for pneumatic actuation
Kuznetsov Y.P., Khimich V.L., Khrunkov S.N., Krainov A.A.
Design of gating systems in production of gas turbine engine blades
Smykov A.F., Moiseev V.S., Chumadin A.S.
Study of Mechanical Properties Stability in the Production of Turbine Disks for Gas Compressor Units
Protasova N.A., Velikanova N.P., Velikanov P.G., Akhmadeev A.A., Salih I.S.
Algorithm of Numerical Checking Calculation of Turbine Cooled Blades of Gas Turbine Engines Using Experimental Data on Heat Transfer and Resistance
Il’inkov A.V., Ermakov A.M., Takmovtsev V.V., Shchukin A.V., Erzikov A.M.
Dynamic behavior of the gas turbine engine regenerator with complanar channels
Trushin V.
Weight optimization principles for turbine blade shroud platform
Belousov A.I., Nazdrachev S.V.
Axial Gas-Dynamic Forces in a Compact Centrifugal Compressor
Evgen’ev S.S., Futin V.A.
Trends in research of hydrodynamic damping in rotor supports of gas turbine engines
Falaleev S.V.
Analysis of the Impact of Fan Blade Geometric Deviations on the Strength Properties
Arkhipov A.N., Volgina M.V., Matushkin A.A., Ravikovich Y.A., Kholobtsev D.P.
To Solution of the Optimization Problem for the Small Dimension Engine Core Turbine Wheel Space
Remizov A.E., Vyatkov V.V., Osokina E.S., Kharchenko R.V.
A Method of Working Process Parameter Optimization of a Unified Engine Core and a Gas Turbine Engine Family Being Created on Its Basis
Rybakov V.N., Kuz’michev V.S., Tkachenko A.Y., Krupenich I.N.
Analysis of cleaning technology for gas turbine engine oil systems as a stage of product life cycle
Tuktamysheva Y.A., Tuktamyshev V.R.
Graph Modeling of Data for Assembly Process of GTE Units in Conditions of Production Digitalization
Lyutov A.G., Ryabov Y.V., Akh’yanillin N.I., Davletshin L.I.
Analysis of Factors Affecting the Service Life of a Centripetal Turbine Rotor
Trushin V.A.
A technique for numerical modeling of liquid film disintegration in the pneumatic injector of aircraft engines
Kolodyazhnyi D.Y., Nagornyi V.S., Sipatov A.M., Modorskii V.Y.
A Method of Calculating the Small-Sized Combustion Chambers
Lanskii A.M., Lukachev S.V., Matveev S.G., Kolomzarov O.V.
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