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Experimental method for evaluating the balance of high-speed small-sized internal combustion engines
Rekadze P.D., Sychugov S.Y., Melentiev V.S., Rodionov L.V.
Experimental determination of damping coefficient of a support with elastic ring under harmonic loading
Diligenskiy D.S., Lezhin D.S., Novikov D.K., Luo C.
Development of hydraulic devices with elastic regulating elements
Berestovitsky E.G., Gladilin Y.F., Pyalov N.V.
Generation of signals with prescribed spectral characteristics
Baraboshin A.Y., Minaeva O.A.
Generation of control programes for disposable unmanned aircraft vehicle propulsion system by means of dynamic characteristic
Mikhailov A.Y., Akhmedzyanov D.A., Akhmetov Y.M., Mikhailova A.B.
Efficiency of using electric propulsion engines for the task of keeping in a near-circular orbit
Ishkov S.A.
Assessing weight efficiency of carrier rockets launched from dirigibles and airplanes
Kurenkov V.I.
Approximation of characteristics of linear displacement inductive sensors using modified Gaussian function with a first order difference argument
Tingaev V.S., Matyunin S.A., Mednikov V.A.
Theoretical calculation approach of gas turbine engines compressor characteristic line
1 1.
Pilot study of frequency characteristics of an acoustic probe for measuring pressure pulsations in the gas turbine engine inlet device
Ivanenko V.N., Alexandrova T.G., Dyagileva E.C., Gimadiyev A.G., Bystrov N.D.
Oxyhydrogen propulsion device base on water electrolysis and lrest on component H2 + O2 for control system SS
1 1., 1 1., 1 1., 1 1., 1 1.
Calculation of basic parameters of spring unloading and shock-proof devices of all-metal multicomponent dampfers on material МR basis
Lazutkin G.V., Parovay F.V., Petukhova M.A., Troynikov A.A.
The use of mathematical optimization means to increase the efficiency of a seven-stage axial flow compressor
Baturin O.V., Popov G.M., Gorachkin E.S., Novikova Y.D.
Development of the finite element model of vibroacoustical characteristics of pipe system
Mironova T.B., Prokofiev A.B., Shahmatov E.V.
Turboprofan jet modeling and equivalent specific fuel consumption optimization subsystem construction on the seminatural modelling stand
Pogorelov G.I., Krivosheev I.A., Godovanyuk A.G., Danilin O.E., Badamshin B.I.
Optimization of model positional harakterstik of the electromagnetic sensor of the linear peremeshchny
Tingaev V.S., Matyunin S.A., Mednikov V.A.
Study of flow characteristics in straight-flow combustion chamber with sudden expansion
Egorov A.G., Zotkin V.I., Ivanin S.V.
Mixing processe research in 10…15 N thrusters
Salich V.L., Semkin E.V.
Aerodynamic improvement of GTE compressors by space profiling of blade vanes
Gerasimenko V.P., Shelkovsky M.Y.
Choosing the form of space vehicle designed for descent in the rarefied atmosphere of Mars
Aslanov V.S., Ledkov A.S.
Modal analysis of the dynamic mockup of “AIST–2D” small spacecraft
Igolkin A.A., Safin A.I., Filipov A.G.
Device for removing phasefrequency characteristics amplifiers
Tyulevin S.V., Piganov M.N., Chopin G.P., Elizarov S.V.
1 - 22 of 22 Items

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