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The adjustment of the mathematical model accuracy of the gas-hydraulic flight control actuator power circuit of an aircraft
Ermakov S.A., Lalabekov V.I., Samsonovich S.L.
A method of design calculation for the two-component jet-jet gas nozzle with outer mixing
Egorychev V.S., Ryazanov A.I.
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.
Numerical Research of Intra-Chamber Transient Processes Dynamics during Starting Operation of the Solid Propellant Rocket Engine with Special Arrangement
Egorov M.Y.
Concepts of Gas Turbine Engine Improvement Through the Use of Choked-Flow Turbines
Bogdanov V.I.
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.
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.
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.
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.
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.
Influence of Boundary Conditions on Characteristics of the Two-Phase Double-Circuit Coaxial Jet in Its Initial Section
Zuev Y.V.
Influence of the disperse phase properties on characteristics of the shock wave passing the direct shock from pure gas in the gas mixture
Gubaidullin D.A., Tukmakov D.A.
A technique of gaseous fuel and air mixture quality identification behind the swirl burner of gas turbine engine combustion chamber
Baklanov A.V., Neumoin S.P.
Development of the design scheme of cooling for a nozzle vane of high pressure turbine of gas turbine engine
Vikulin A.V., Yaroslavtsev N.L., Chesnova V.A.
A Method of Calculating the Small-Sized Combustion Chambers
Lanskii A.M., Lukachev S.V., Matveev S.G., Kolomzarov O.V.
Calculation of the Fuel Gas Heating in the Flame Tube Head of Multi-Injector Combustion Chamber of the Gas Turbine Engine
Baklanov A.V., Malyukov A.V.
Numerical Simulation of Detachment Dynamics of a Payload from the Parent Aircraft
Bykov L.V., Pashkov O.A., Pravidlo M.N., Tishkov V.V., Yanyshev D.S.
Calculation of low cycle fatigue life for gas-turbine engine critical parts
Pakhomenkov A.V., Azimov R.A., Bukatyi S.A.
On similarity criteria in flight mechanics
Golovkin M.A., Deryabin E.Y.
Study of Heat Transfer from the Shell of Gas Turbine Plant and Methods of Its Thermal Protection
Baklanov A.V., Gimbitskii A.V.
Numerical Simulation of Shock-Wave Flows in a Gas Suspension with Inhomogeneous Concentration of the Dispersed Phase
Tukinakov D.A.
Axial Gas-Dynamic Forces in a Compact Centrifugal Compressor
Evgen’ev S.S., Futin V.A.
Wear and Erosion Resistance of Aircraft Engine Composite Elements in a Gas Abrasive Flow
Zinin A.V., Dobrovol’skii S.V., Lebedev A.K., Krupennikov V.A., Shevyakov A.O.
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.
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.
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