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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., Kuz’michev V., Tkachenko A., Krupenich I.
Concepts of Gas Turbine Engine Improvement Through the Use of Choked-Flow Turbines
Bogdanov V.
Estimation of mode onset for reverse jet reattachment to the engine nacelle in a flow
Varsegov V.
Changes in the Cruise Climb Performance of the Il-96-300 Aircraft
Maslennikova G., Arep’ev K., Tazhetdinov R., Nikonov V., Spryskov V.
Static Stability in the Angular Motion of an Aircraft with a Laser-Induced Spike Conical Nozzle
Sattarov A., Sochnev A., Bikmuchev A.
Probabilistic Assessment of Life for Gas Turbine Engine Parts Considering Manufacture Tolerances
Arkhipov A., Volgina M., Matushkin A., Ravikovich Y., Kholobtsev D.
Graph Modeling of Data for Assembly Process of GTE Units in Conditions of Production Digitalization
Lyutov A., Ryabov Y., Akh’yanillin N., Davletshin L.
Simulation of a Rocket Engine Nozzle Discharge Coefficient
Sabirzyanov A., Glazunov A., Kirillova A., Titov K.
Numerical Research of Intra-Chamber Processes Dynamics during Startup of a Special Solid Propellant Engine
Egorov M.
Influence of combustion chamber geometry and compression ratio on the main parameters of a diesel aircraft engine
Gureev V., Khairullin A., Varlamov F., Gumerov I., Khafizov R.
Influence of exhaust gas recirculation on technical, economic, and environmental performance of high-uprated diesel aircraft engine
Gureev V., Khairullin A., Varlamov F., Gumerov I., Khafizov R.
Optimization of the Stage Number and Parameter Distribution in the Flow Passage at GTE Compressor and Turbine Design
Krivosheev I., Rozhkov K., Simonov N.
Integration of a High-Pressure Gas Turbine of the Gas Turbine Engine with a Gas-Dynamic Laser
Perel’shtein B., Osipov B., Titov A.
On the Ballistic Efficiency of Bicalibre Aerial Vehicles with Prevailing Coast Phase
Vetrov V., Gusev A., Kuznetsov V., Dikshev A., Kostyanoi E.
Influence of the helicopter flight design speed on the selection of working process parameters for GTE
Grigor’ev V., Zagrebel’nyi A.
Research and Development of the Joint Seals for Gas Turbine Engine High-Temperature Turbine Stator Units
Belousov A., Borisov V., Parovai F.
Problem of the Community Noise Reduction for Aircraft with Open Rotor Engines
Moshkov P., Samokhin V., Yakovlev A.
Use of a Nonlinear Mathematical Model of Turboprop Engine on a Semi-Full-Scale Simulation Test Bench for Testing Propellers in Conjunction with Their Automatic Control System
Ivanov A., Danilikhin A., Baranov V.
Study of performance of the aircraft gas turbine engine integrated with a gas dynamic laser
Osipov B., Kopelevich L., Perel’shtein B.
Numerical determination of the gas-dynamic behavior of vane cascades with various deflection angles of the trailing edges of longitudinal ribs of an advanced gas-turbine engine thrust reverser
Varsegov V., Shabalin A.
Electric charge imposition on hydrocarbon fuel drops in sharply inhomogeneous electric field of injector modules
Kolodyazhnyi D., Nagornyi V.
Extreme Triple Configurations with Negative Slope Angle of the Reflected Shock
Chernyshov M.
The Concept of a Small-Size Guided Air-to-Surface Missile with Paste-Like Propellant Rocket Engine
Kabanov D., Makhrov V.
Axial Gas-Dynamic Forces in a Compact Centrifugal Compressor
Evgen’ev S., Futin V.
Calculation of low cycle fatigue life for gas-turbine engine critical parts
Pakhomenkov A., Azimov R., Bukatyi S.
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