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Thermal control of spacecraft star sensor attitude control system based on the solution of a coupled thermoelasticity problem
Tsaplin S.V., Bolychev S.A.
Automated generation of structural members of a spacecraft thermal model
Kulikov D.S., Shatin A.A., Velmisov I.G.
Investigation of thermal conditions of nanosatellite optoelectronic telescopic module for different modes of operation
Tsaplin S.V., Bolychev S.A.
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.
Centrifugal force field effect consideration in dynamics investigation of blade wheels
Davydov D.P., Ermakov A.I.
Influence of argon, propane and ethane viscous dissipation on the thermal state of a porous plate
Baygaliev B.E., Tumakov A.G., Tumakov E.A., Ibragimov A.I.
Results of hot tests of an oxygen preburner of a liquid-propellant engine 11D58MF
Barsukov O.A., Strizhenko P.P.
Peculiarities of gas temperature field formation at the exit of small-sized gas turbine engine combustion chambers
1 1., 1 1., 1 1.
Investigation of the thermal regime of microsatellite optoelectronic telescopic complex under operating conditions
Tsaplin S.V., Bolychev S.A.
Mathematical model for calculating radial non-uniformity of the gas temperature field at the exit of small gas turbine engine combustion chambers
Lukachev S.V., Abrashkin V.Y., Lansky A.M., Matveev S.G.
Methodology of optimization of parameter of matching the combustion chamber and turbine joint operation
Grigoriev A.V., Golubchikov P.P., Ilushin M.Y., Rudakov O.A., Solovieva 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.
Use of control volume method for the temperature field calculation by laser influence
Murzin S.P., Mezhenin A.V., Osetrov E.L.
Conditions of compatibility of compressor and turbine used as part of a gas generator required to ensure turbine operability
Grigoriev A.V., Ilyushin M.Y., Mitrofanov V.A., Rassokhin V.A., Rudakov O.A., Solovieva A.V.
1 - 14 of 14 Items

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