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Modeling of convective heat transfer processes between inhomogeneous gas mixtures and surfaces of a small-caliber artillery barrel
Podkopaev I.A., Podkopaev A.V., Dolzhikov V.I.
Heat transfer in the centrifugal force field for gas turbines elements
Zuev A.A., Arngold A.A., Khodenkova E.V.
Determining thermal resistance in the model of the liquid circuit of spacecraft thermal control system
Shevchenko Y.N., Kishkin A.A., Tanasienko F.V., Shilkin O.V., Popugayev M.M.
Increasing the specific impulse of an oxygen-hydrogen liquid rocket engine by increasing heat transfer in the combustion chamber
Vasilevsky D.O.
Calculation of complex heat transfer in the liquid circuit of the spacecraft thermal control system based on real topology and thermophysical properties
Shevchenko Y.N., Kishkin A.A., Tanasienko F.V., Shilkin O.V., Sokolov S.N.
Design of the cooling system of a reasuble liquid rocket engine with three-component fuel
Belyakov V.A., Vasilevsky D.O., Ermashkevich A.A., Kolomentsev A.I., Farizanov I.R.
Local heat transfer parameters in the areas of the developing temperature boundary layer in the cavities of gas turbines local heat transfer parameters in the areas of the developing temperature boundary layer in the cavities of gas turbines
Zuev A.A., Arngol'd A.A., Falkova E.V., Tolstopyatov M.I., Dubynin P.A.
Identification and simulation mathematical model of thermo and physical loading of a small-caliber artillery barrel
Podkopaev A.V., Babadzanov A.B., Podkopaev I.A., Dolzhikov V.I.
ROTATIONAL FLOWS HEAT TRANSFER IN TURBOMACHINES BASED ON TWO-LAYER MODEL OF TURBULENT BOUNDARY LAYER
Zuev A.A., Kishkin A.A., Tolstopyatov M.I., Zhuykov D.A.
INSTALLATION FOR EXPERIMENTAL RESEARCH OF CONVECTIVE HEAT OF THE ROTATIONAL GAS FLOW
Zuev A.A., Tolstopyatov M.I., Zhuikov D.A.
COMPUTATIONAL EXPERIMENT ON OBTAINING THE CHARACTERISTICS OF A THERMAL CONTROL SYSTEM OF SPACECRAFT
Tanasienko F.V., Shevchenko Y.N., Delkov A.V., Kishkin A.A., Melkozerov M.G.
THE STUDY OF THE FLOW IN THE VAPOUR CHANNEL OF SHORT LINEAR HEAT PIPES
Seryakov A.V.
DISTRIBUTED PARAMETERS ENERGY-HEAT MODEL OF SPACE NICKEL-HYDROGEN STORAGE BATTERY
Sakhnov M.Y., Lelekov A.T., Galochkin S.A., Sahnov M.Y., Lelekov A.T., Galochkin S.A.
HEAT TRANSFER IN THE CAVITY OF A GAS TURBINE LIQUID ROCKET ENGINE
Zuev A.A., Tolstopyatov M.I.
MODELING OF THERMAL OBJECTS WITH DISTRIBUTED PARAMETERS WITH THE USE OF COMSOL MULTIPHYSICS-MATLAB-SIMULINKSOFTWARE PACKAGES
Lelekov A.T., Sakhnov M.Y., Galochkin S.A., Velichko E.V., Lelekov A.T., Sahnov M.Y., Galochkin S.A., Velichko E.V.
MODELING OF SPECTROERERGETIC CHARACTERISTICS OF SPACE OBJECTS IN THE OPTICAL RANGE
Bogoyavlenskiy A.I., Kamenev A.A., Poluyan M.M., Soluyanov A.A.
NUMERICAL SIMULATION OF MODIFYING MATERIAL DISTRIBUTION DURING THE IMPULSE INDUCTION HEATING OF METAL SURFACE
Popov V.N.
BUNDLED SOFTWARE TO COMPUTE TEMPERATURE FIELDS OF SPACE VEHICLES PANELS WITH LEAKY CONSTRUCTION
Vasiljev E.N., Derevyanko V.V.
Calculation of eigenvalues in the problem of unsteady heat transfer through a cylindrical wall with mixed boundary conditions
Vidin Y.V., Ivanov D.I.
1 - 19 of 19 Items

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