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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.
Investigation of the Flow Mixing behind the Flame Tube Head of a Combustion Chamber in a Gas Turbine Engine
Sulaiman A.I., Mingazov B.G., Aleksandrov Y.B., Nguen T.D.
Numerical simulation of the flow in the rotation cavities of turbopump assembly
Zhuikov D.A., Nazarov V.P.
Analyzing and Ensuring the Dynamic Accuracy of the Aircraft Air Data System with a Fixed Flush-Mounted Flow Receiver
Soldatkin V.M., Soldatkin V.V., Nikitin A.V., Kornilov V.Y.
Mechanism of transport phenomena at low pressures
Panfilovich K.B.
Fluid film break-up modeling using adaptive mesh refinement models
Sipatov A.M., Karabasov S.A., Gomzikov L.Y., Abramchuk T.V., Semakov G.N.
Mathematical Model of the Flow of a Liquid Film of Variable Thickness on a Flat Surface in a Viscous Gas Flow
Klyuev N.I., Polyakov K.A.
Fuel atomization and mixing in unsteady swirling flows behind the gas-dynamic stabilizer
Tret’yakov V.V., Sviridenkov A.A., Toktaliev P.D.
Wave resistance defect in a planar flow over periodic reliefs
Semenov V.V., Volkov V.A., Kwon M.C., Sidhu J.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.
Aerodynamic Characteristics of Thin Cylindrical and Conical Shells in the Incompressible Flow
Kalugin V.T., Lutsenko A.Y., Nazarova D.K.
Analysis of hydrodynamic unsteady turbulent flow structure in an aircraft power plant channels
Kraev V.M., Myakochin A.S.
Collapse of a spheroidal cavitation bubble near a solid wall
Aganin A.A., Il’gamov M.A., Kosolapova L.A., Malakhov V.G.
Design Features and Efficiency Analysis of the Aircraft Complex Air Data System with a Fixed Flush-Mounted Flow Receiver
Soldatkin V.M.
To the Problem of Friction Minimization on Permeable Surfaces at Supersonic Flow Rate
Garaev K.G., Mukhametzyanov I.R.
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.
Statistical analysis of stretch shaping process of biconvex skin
Mikheev V.A., Smol’nikov S.D., Surudin S.V., Savin D.V.
Heating of an Anisotropic Insulation Layer with Hypersonic Flow Past a Spherical Blunting
Zarubin V.S., Leonov V.V., Zarubin V.S.
Effect of Heat Transfer Surface Shape on Efficiency of Gas Dynamic Temperature Stratification
Tsynaeva A.A., Nikitin M.N.
Numerical scheme of the second order of accuracy for vortex methods for incompressible flow simulation around airfoils
Kuz’mina K.S., Marchevskii I.K., Moreva V.S., Ryatina E.P.
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.
To the Problem of Optimal Thermal Protection of Surfaces in Supersonic Flows
Garaev K.G., Mukhametzyanov I.R.
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.
A method of design calculation for the two-component jet-jet gas nozzle with outer mixing
Egorychev V.S., Ryazanov A.I.
Pressure recovery in a planar diffuser at pulsatory flow regimes
Davletshin I.A., Mikheev N.I., Paerelii A.A.
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