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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.
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.
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.
On Relationship of Flow Swirl Parameters and Gas-Dynamic Efficiency of Gas Turbine Engine Interturbine Transition Duct
Remizov A.E., Vyatkov V.V., Lebedev V.V.
Spatial vibration protection in a turbopump of hydrogen rocket engines
Belousov A.I., Ponomarev Y.K.
Study of Heat Transfer from the Shell of Gas Turbine Plant and Methods of Its Thermal Protection
Baklanov A.V., Gimbitskii A.V.
Vortex Structure Intensity in Diffuser Dimples
Il’inkov A.V., Takmovtsev V.V., Shchukin A.V., Khabibullin I.I., Zaripov I.S.
Probabilistic Assessment of Life for Gas Turbine Engine Parts Considering Manufacture Tolerances
Arkhipov A.N., Volgina M.V., Matushkin A.A., Ravikovich Y.A., Kholobtsev D.P.
Effect of a Model and Boundary Conditions on the Results of Analyzing the Stress-Strain State of a Low-Pressure Compressor Rotor
Arkhipov A.N., Volgina M.V., Matushkin A.A., Ravikovich Y.A., Kholobtsev D.P.
Calculation of low cycle fatigue life for gas-turbine engine critical parts
Pakhomenkov A.V., Azimov R.A., Bukatyi S.A.
A high-temperature frameless starter-generator integrated into an aircraft engine
Ismagilov F.R., Khairullin I.K., Vavilov V.E., Farrakhov D.R., Yakubov A.M., Bekuzin V.I.
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.
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