Peculiarities of modeling the work process in a low-pressure compressor of a gas turbine plant
Matveev V.N., Popov G.M., Goryachkin E.S., Smirnova Y.D.
The influence of burner design on the characteristics of the combustion chamber with gaseous fuels
Markushin A.N., Baklanov A.V., Tsyganov N.E.
Analyzing the quality of preparing fuel-air mixture and its influence on NOx in a low emission gas turbine engine combustion chamber
Markushin A.N., Baklanov A.V.
Test benches for researching the processes and operational development of low emission gas turbine engine combustion chambers
Markushin A.N., Baklanov A.V.
Experimental study of air flow in axisymmetric diffuser output section with rotating wall
Kurkin E.I., Ivchenko A.V.
Computer-aided-design system for calculating adsorption thermodynamic characteristics
Zelenko L.S., Varfolomeyeva V.V., Kuznetsov V.Y., Fed’kayev A.V., Terentyev A.V., Buryak A.K.
Influence of the burner form on the combustion chamber outlet temperature field ripple for different modes of operation of gas turbine engines
Markushin A.N., Baklanov A.V.
Investigation of the gas turbine engine combustion chamber workflow
Markushin A.N., Baklanov A.V.
Numerical investigation of gas dynamics in nozzles of small-dimensioned gas generators and flowing out jets
Ivanov I., Kryukov I., Shustov S.
Choosing the aerodynamic configuration of a subsonic cruise missile
Kovalev M.A., Nikitin A.N.
Experimental analysis of flow separation in low thrust rocket engine nozzles with a profiled supersonic part of the nozzle
Shustov S.A.
Study of characteristics of the vortex throttling valve for the sysytem of water sample conditioning
Gimadiev A.G., Utkin A.V.
Approbation of the numerical model of account of viscosity impact on the flow in low-thrust rocket engine nozzles in the approximation of a laminar boundary layer with sliding
Shustov S.A.
Biological module “BiNOM” for cubesats of the SamSat family
Zakharov V.P., Konyukhov V.N., Bakhtinov P.I., Molchkov E.V., Kornilin D.V., Konovalov S.G.
Complex approach to aerodynamic design of inlet ducts with submerged vortex-free air intakes
Kornev A.V., Boychuk I.P.
Dynamics of the hydromechanical system of a production machine with an adaptive tool-feeding drive
Sidorenko V.S., Poleshkin M.S., Rakulenko S.V.
Experimental study of a power absorber of accelerated fluid flow in pipelines
Gimadiev M.A., Gimadiev A.G.
Structural model of individual forecasting of space radioelectronic equipment parameters
Tyulevin S.V., Piganov M.N.
Experimental determination of acoustic loads daunches of Strela LV and calculation of test modes for a spacecraft to be delivered by it to space
1 1., 1 1., 1 1., 1 1.
Choise of the range and levels of varying the factors of the experiment plan for testing single-stage ultralow power turbine
Grigoryev V.A., Radko V.M., Kalabukhov D.S.
Analysis of the effectiveness of predictive models of quality parameters of the chips
Tyulevin S.V., Arhipov A.I., Piganov M.N., Elizarov S.V.
Modernization of test-bench for small turbine-drives investigation
Matveev V.N., Shabliy L.S.
The development of the optimization methodology of the turbine blade-disk interlock of the type “fir tree”
Bukaty A.S., Bukaty S.A., Andreev I.B.
Development and research of a low-toxic combustion chamber of a stationary GTE
Markushin A.N., Merkushin V.K., Baklanov A.V.
Experiments aboard the space vehicle “Photon-M” NO.3 and some reseelts of the mission
Abrashkin V.I., Shatokhin S.M., Kovalyova T.B., Safronov S.L.
Ground testingresults of loop heat pipe used to maintain thermal conditions of equipment
Biryuk V.V., Kitaev A.I.
Planning a factorial experiment for testing a single-stage ultralow power turbine
Grigoryev V.A., Radko V.M., Kalabukhov D.S.
Mathematical modeling of technological production process of thermo-stable resistor – capacity structures
Merkulov A.I., Laktanov P.V., Merkulov V.A.
Training experiment at forecasting of quality and reliability of soldered joints of electronic assemblages
Shumskikh I.Y., Tyulevin S.V.
1 - 29 of 29 Items

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