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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.
Changes in the Cruise Climb Performance of the Il-96-300 Aircraft
Maslennikova G.E., Arep’ev K.A., Tazhetdinov R.R., Nikonov V.V., Spryskov V.B.
Static Stability in the Angular Motion of an Aircraft with a Laser-Induced Spike Conical Nozzle
Sattarov A.G., Sochnev A.V., Bikmuchev A.R.
Concepts of Gas Turbine Engine Improvement Through the Use of Choked-Flow Turbines
Bogdanov V.I.
Estimation of mode onset for reverse jet reattachment to the engine nacelle in a flow
Varsegov V.L.
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.
Stability of Decisions in Choosing the Operating Parameter Values of the Gas Turbine Engine in the Helicopter System at the Initial Design Stage
Grigor’ev V.A., Zagrebel’nyi A.O.
Influence Analysis of the Second Bypass Air Bleed Parameters on the Engine Performance
Agul’nik A.B., Kravchenko I.V., Gorbunov A.A., Novoselova A.A., Sklyarova A.P.
The 3D Computational Investigation of Film Cooling Effectiveness for Turbine Nozzle Vanes with “Meridian Constriction” and Shaped Film-Cooling Holes
Gorelov Y.G., Tyul’kov K.V.
Problems and prospects of using gas and hydrodynamic lubricants in support seals of aircraft engine rotors
Balyakin V.B.
Roll control of a flight vehicle with the adjustable center of mass
Afanas’ev V.A., Degtyarev G.L., Kiselev V.I., Meshchanov A.S.
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.
The Concept and Definition of Integrated Flight Performance for a Small Remotely Piloted Helicopter
D’yakonov D.A., Zavalov O.A., Turkin I.K.
Trends in research of hydrodynamic damping in rotor supports of gas turbine engines
Falaleev S.V.
The adjustment of discharge and spray in fuel injectors of aircraft engines
Smolentsev V.P., Safonov S.V., Koptev I.I.
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.
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.
Simulation of a Rocket Engine Nozzle Discharge Coefficient
Sabirzyanov A.N., Glazunov A.I., Kirillova A.N., Titov K.S.
Numerical Research of Intra-Chamber Processes Dynamics during Startup of a Special Solid Propellant Engine
Egorov M.Y.
Influence of combustion chamber geometry and compression ratio on the main parameters of a diesel aircraft engine
Gureev V.M., Khairullin A.K., Varlamov F.A., Gumerov I.F., Khafizov R.K.
Influence of exhaust gas recirculation on technical, economic, and environmental performance of high-uprated diesel aircraft engine
Gureev V.M., Khairullin A.K., Varlamov F.A., Gumerov I.F., Khafizov R.K.
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.
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.
On the Ballistic Efficiency of Bicalibre Aerial Vehicles with Prevailing Coast Phase
Vetrov V.V., Gusev A.V., Kuznetsov V.M., Dikshev A.I., Kostyanoi E.M.
Influence of the helicopter flight design speed on the selection of working process parameters for GTE
Grigor’ev V.A., Zagrebel’nyi A.O.
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