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Numerical simulation of the flow in the rotation cavities of turbopump assembly
Zhuikov D., Nazarov V.
Optimization of the Stage Number and Parameter Distribution in the Flow Passage at GTE Compressor and Turbine Design
Krivosheev I., Rozhkov K., Simonov N.
Investigation of the Flow Mixing behind the Flame Tube Head of a Combustion Chamber in a Gas Turbine Engine
Sulaiman A., Mingazov B., Aleksandrov Y., Nguen T.
Design Features and Efficiency Analysis of the Aircraft Complex Air Data System with a Fixed Flush-Mounted Flow Receiver
Soldatkin V.
To the Problem of Friction Minimization on Permeable Surfaces at Supersonic Flow Rate
Garaev K., Mukhametzyanov I.
A technique for numerical modeling of liquid film disintegration in the pneumatic injector of aircraft engines
Kolodyazhnyi D., Nagornyi V., Sipatov A., Modorskii V.
Statistical analysis of stretch shaping process of biconvex skin
Mikheev V., Smol’nikov S., Surudin S., Savin D.
Heating of an Anisotropic Insulation Layer with Hypersonic Flow Past a Spherical Blunting
Zarubin V., Leonov V., Zarubin V.
Effect of Heat Transfer Surface Shape on Efficiency of Gas Dynamic Temperature Stratification
Tsynaeva A., Nikitin M.
Numerical scheme of the second order of accuracy for vortex methods for incompressible flow simulation around airfoils
Kuz’mina K., Marchevskii I., Moreva V., Ryatina E.
Wear and Erosion Resistance of Aircraft Engine Composite Elements in a Gas Abrasive Flow
Zinin A., Dobrovol’skii S., Lebedev A., Krupennikov V., Shevyakov A.
To the Problem of Optimal Thermal Protection of Surfaces in Supersonic Flows
Garaev K., Mukhametzyanov I.
On Relationship of Flow Swirl Parameters and Gas-Dynamic Efficiency of Gas Turbine Engine Interturbine Transition Duct
Remizov A., Vyatkov V., Lebedev V.
A method of design calculation for the two-component jet-jet gas nozzle with outer mixing
Egorychev V., Ryazanov A.
Pressure recovery in a planar diffuser at pulsatory flow regimes
Davletshin I., Mikheev N., Paerelii A.
Solution of One Classical Gas Dynamics Problem
Efimov A.
Application of the DRGEP and Engagement Methods to Reduce the Reaction Mechanisms for Calculation of Chemically Non-Equilibrium Flows in Aircraft Engine Nozzles
Krioukov V., Abdullin A., Nikandrova M., Safiullin I.
Influence of Simplifying a Geometrical Model of the Gas Turbine Engine Combustion Chamber on the Results of Numerical Modeling
Aleksandrov Y., Sabirzyanov A., Yavkin V.
Improvement of gas-dynamic efficiency of GTE gas turbine stages at the design stage
Remizov A., Vyatkov V., Lebedev V.
Near-Wall Heat and Mass Transfer in a Channel behind a Rib
Dushin N., Mikheev N., Dushina O., Davletshin I., Zaripov D.
Vortex Structure Intensity in Diffuser Dimples
Il’inkov A., Takmovtsev V., Shchukin A., Khabibullin I., Zaripov I.
Determination of Gas-Generator Fuel Capacity for Hybrid Aerial Underwater Vehicles with Airfoil Cavity-Forming System
Makhrov V., Sorokin V., Yur’ev A.
Parabolic convective motion of a fluid cooled from below with the heat exchange at the free boundary
Vlasova S., Prosviryakov E.
Analyzing and Ensuring the Dynamic Accuracy of the Aircraft Air Data System with a Fixed Flush-Mounted Flow Receiver
Soldatkin V., Soldatkin V., Nikitin A., Kornilov V.
Mechanism of transport phenomena at low pressures
Panfilovich K.
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