Issue
Title
Authors
Modeling of dynamic processes in micromechanical inertial sensors and their components using specialized software
Barulina M.A., Pankratov V.M.
Numerical simulation of tonal noise of a bypass engine fan stage
Pyatunin K.R., Arharova N.V., Remizov A.E.
Development of methods of designing modern gas turbines
Inozemtsev A.A., Khairulin V.T., Tikhonov A.S., Samokhvalov N.Y.
Numerical simulation of gas temperature spatial distribution in a one-burner sector of a gas turbine combustor with uncertain initial conditions of fuel atomization
Kostyuk V.Y., Kirilash Y.I., Stasyuk A.V., Shein V.V., Karzov D.V.
Numerical simulation of the working process in a vortex tube with an additional stream
Vasilyuk O.V., Piralishvili S.A., Shaykina A.A.
Effect of non-uniform compressor flow parameters on the characteristics of a gas turbine engine combustion chamber
Matveev S.G., Orlov M.Y., Zubrilin I.A., Matveev S.S., Tsybizov Y.I.
Influence of the turbine ignition, flame tube suspension and nozzles on the combustion chamber characteristics
Matveev S.G., Orlov M.Y., Zubrilin I.A.
Determination of thermal state and modification of the flame tube cooling system with the help of three-dimensional modeling methods
Matveev S.G., Anisimov V.M., Zubrilin I.A., Kolomzarov O.V., Mironov N.S.
Combined calculation of gas generators of small GTE in package ANSYS CFX
Matveev S.G., Orlov M.Y., Matveev S.S., Zinkovskii V.S., Krivtsov A.V.
Numerical simulation of gas temperature spatial distribution in a full-size gas turbine combustor and its one-burner sector
Kostyuk V.Y., Kirilash Y.I., Stasyuk A.V., Shein V.V., Karzov D.V.
Multi-time-step scheme in the vorticity splitting method applied to the simulation of the wake behind the flat plate
Nikonov V.V., Shakhov V.G.
Synthesis of dynamic modes of attitude motion of spacecraft with solid propellant rocket engine
Balakin V.L., Doroshin A.V., Krikunov M.M.
Dissipative structures of the Gierer-Meinhardt model of morphogenesis in the stochastic field
Kurushina S.E.
Investigation of the causes of the auger-centrifugal pump bearing destruction
Gafurov S.A., Rodionov L.V., Shahmatov E.V.
Influence of the geometry fidelity of resonant sound-absorbing liner samples on their acoustic characteristics
Kustov O.Y., Khramtsov I.V., Bulbovich R.V.
Impact of the turbulence modeling approach on the accuracy of the fan noise level prediction
Pyatunin K.R., Arkharova N.V.
Determination of large-size liner impedance based on numerical simulation of sound propagation in a duct with specified azimuthal modal structure
Korin I.A., Palchikovskiy V.V., Pavlogradskiy V.V.
Improvement of gas turbine engines due to isothermal expansion in the turbine
Muraeva M.A., Gorjunov I.M.
Unstady heat-mass-transfer and fuel distributions in flows downstream the gas-dynamic flame holder
Tretyakov V.V., Sviridenkov A.A.
Study of characteristics of the vortex throttling valve for the sysytem of water sample conditioning
Gimadiev A.G., Utkin A.V.
Specifying the dimensions of the reverse current area of a 3-D gas-turbine engine combustion chamber model using the ANSYS FLUENT software
Biryuk V.V., Orlov M.Y., Zubrilin I.A., Sinegovskiy Y.A., Krivtsov A.V.
Mathematical modeling of the process of selective laser melting of Ti-6Al-4V titanium alloy powder
Agapovichev A.V., Sotov A.V., Smelov V.G.
The numerical modelling of processes in combustion chambers of low thrust rocket engines
Salich V.L.
Development of advanced low thrust rocket engines with ecologically friendly propellants
1 1., 1 1., 1 1.
Mixing processe research in 10…15 N thrusters
Salich V.L., Semkin E.V.
Obliteration’s problems in capillary-porous structures of aerospace hydro systems’ parts
1 1., 1 1.
1 - 26 of 26 Items

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