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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.
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.
Problem of the Community Noise Reduction for Aircraft with Open Rotor Engines
Moshkov P.A., Samokhin V.F., Yakovlev A.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.V., Danilikhin A.M., Baranov V.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.
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.L., Shabalin A.S.
Electric charge imposition on hydrocarbon fuel drops in sharply inhomogeneous electric field of injector modules
Kolodyazhnyi D.Y., Nagornyi V.S.
Extreme Triple Configurations with Negative Slope Angle of the Reflected Shock
Chernyshov M.V.
The Concept of a Small-Size Guided Air-to-Surface Missile with Paste-Like Propellant Rocket Engine
Kabanov D.E., Makhrov V.P.
Axial Gas-Dynamic Forces in a Compact Centrifugal Compressor
Evgen’ev S.S., Futin V.A.
Calculation of low cycle fatigue life for gas-turbine engine critical parts
Pakhomenkov A.V., Azimov R.A., Bukatyi S.A.
Analysis of cleaning technology for gas turbine engine oil systems as a stage of product life cycle
Tuktamysheva Y.A., Tuktamyshev V.R.
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.
Numerical Research of Intra-Chamber Transient Processes Dynamics during Starting Operation of the Solid Propellant Rocket Engine with Special Arrangement
Egorov M.Y.
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.
A Computational Technique for Estimating the Nitrogen Oxide Concentration in Combustion of Air-Fuel Mixture Enriched with Hydrogen in Exhaust Gases of Spark-Ignition Engines
Shaikin A.P., Ivashin P.V., Deryachev A.D.
Design of gating systems in production of gas turbine engine blades
Smykov A.F., Moiseev V.S., Chumadin A.S.
Difference schemes in computations for chemically non-equilibrium processes in the rocket engine nozzles
Kryukov V.G., Abdullin A.L., Demin A.V.
Simulation of thermal radiation emitted by heterogeneous combustion products in the combustion chamber of a model engine
Kuz’min V.A., Maratkanova E.I., Zagrai I.A., Rukavishnikova R.V.
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