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Determining aerodynamic characteristics of small unmanned aerial vehicles involving flight experiment
Lukyanov O.E., Zolotov D.V., Espinosa Barsenas O., Komarov V.A.
Experimental and analytical determination of the elastic characteristics of layered woven composites
Komarov V.A., Pavlov A.A., Pavlova S.A.
Experimental analysis of instability and self-oscillations in an electrohydraulic servo drive
Petrov P.V., Sunarchin R.A., Mashkov M.A., Krivosheev N.S.
Main approaches and features of the design of aircraft hydro-mechanical control systems
Petrov P.V., Tselischev V.A., Kuderko D.A.
Special features of assessing the strength of nuclear reactor equipment under dynamic loads
Lonin K.A., Panov V.A., Patrushev V.L., Savchuk D.V., Soloviev S.A.
Mathematical modeling of technological production process of thermo-stable resistor – capacity structures
Merkulov A.I., Laktanov P.V., Merkulov V.A.
Development of methods of carrying out experimental research of measurement errors for sets of geometrical parameters on NC equipment as in the case of a turbine disk
Bolotov M.A., Alexeev V.P., Pronichev N.D.
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.
Structural model of individual forecasting of space radioelectronic equipment parameters
Tyulevin S.V., Piganov M.N.
Professor A.P. Merkulov’ role in the process of research and development of the vortex effect
Biryuk V.V., Lukachev S.V., Volov V.T., Pirallishvili S.A.
Training experiment at forecasting of quality and reliability of soldered joints of electronic assemblages
Shumskikh I.Y., Tyulevin S.V.
Research of shaft seals made of porous wire «metal rubber» material
Zhizhkin A.M., Zrelov V.A., Zrelov V.V., Ardakov A.Y., Osipov A.A.
Technical solutions of NOx decrease in traditional combustion chamber of GTE NK-16ST
Markushin A.N., Merkushin V.K., Byshin V.M., Baklanov A.V.
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.
Choosing the aerodynamic configuration of a subsonic cruise missile
Kovalev M.A., Nikitin A.N.
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.
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.
Experimental analysis of flow separation in low thrust rocket engine nozzles with a profiled supersonic part of the nozzle
Shustov S.A.
Test benches for researching the processes and operational development of low emission gas turbine engine combustion chambers
Markushin A.N., Baklanov A.V.
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.
Study of characteristics of the vortex throttling valve for the sysytem of water sample conditioning
Gimadiev A.G., Utkin A.V.
Development of discrete pneumatic pressure regulator and researching of its characteristics
Greshniakov P.I., Sinyakov A.F., Ilukhin V.N.
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.
Development and analysis of screw restrictor hydraulic characteristics in the air bleed valve control unit of a gas turbine engine
Gimadiev A.G., Makaryants G.M., Blyumin K.V., Dudnichenko I.M.
Experimental study of a power absorber of accelerated fluid flow in pipelines
Gimadiev M.A., Gimadiev A.G.
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.
Complex approach to aerodynamic design of inlet ducts with submerged vortex-free air intakes
Kornev A.V., Boychuk I.P.
Application of stereolithography prototypes for gas dynamic tests
Matveev V.N., Shabliy L.S., Krivcov A.V.
Experimental study of air flow in axisymmetric diffuser output section with rotating wall
Kurkin E.I., Ivchenko A.V.
Study of flow characteristics in straight-flow combustion chamber with sudden expansion
Egorov A.G., Zotkin V.I., Ivanin S.V.
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.
Development and research of a low-toxic combustion chamber of a stationary GTE
Markushin A.N., Merkushin V.K., Baklanov A.V.
The influence of burner design on the characteristics of the combustion chamber with gaseous fuels
Markushin A.N., Baklanov A.V., Tsyganov N.E.
Ground testingresults of loop heat pipe used to maintain thermal conditions of equipment
Biryuk V.V., Kitaev A.I.
Investigation of the gas turbine engine combustion chamber workflow
Markushin A.N., Baklanov A.V.
Experimental studies of shell vibrations
Lezhin D.S., Nagurnaya O.V., Nikulin E.V., Vergnano D.
Numerical investigation of gas dynamics in nozzles of small-dimensioned gas generators and flowing out jets
Ivanov I., Kryukov I., Shustov S.
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.
1 - 39 of 39 Items

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