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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.
Numerical and experimental study of the strength of fabric carbon-epoxy composite structures
Komarov V.A., Kishov E.A., Charkviani R.V., Pavlov A.A.
Processing of experimental data by the method of the least squares
Ovchinnikov A.V., Krasnochub E.K., Bronstein V.M.
Technique of conclusion the direct-flow detonation pulsing engine design to the leader position
Safronov V.V., Porshnev V.A., Zhebrakov A.S.
Problems of ultralow power turbine design in a turbine drive system
Kalabuhov D.S., Grigoryev V.A., Rad’ko V.M.
Use of the mathematical tool of hypervector ranging for selection energy-power plant of flight vehicles
Safronov V.V., Zhebrakov A.S.
Implementation of control technigue for institute of higher technological education students' self-educational activity
Tarabrina T.B.
Multicriterial choice of the best variant of the pulse detonation engine design for aircraft angular stabilization and orientation systems
Safronov V.V., Porshnev V.A., Zhebrakov A.S.
Methods and models of autonomous control over Earth remote sensing spacecraft survivability
Akhmetov R.N.
Features of optimization of the versatile gas generator parameters and design for development of a broad power range line of the advanced gas turbine engines of different application
Sharova N.A.
Energy optimality criteria
Danilin A.I.
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.
Methodological and analytical support for the creation and maintenance of aerospace industry technological development strategic programs
Gaponenko O.V.
Mathematical models of optimal investment control in fixed assets
Pavlov O.V., Moshkova T.A.
Criterion assessment of the possibility to prolong the service life limit of the helicopter tail drive shaft
Mashoshin O.F., Semenikhin R.L.
Processing of experimental data by the method of the least squares
1 1., 1 1., 1 1.
Mathematical models for evaluating the energy efficiency of ultralow power turbine drives
Kalabuhov D.S., Grigoryev V.A., Rad’ko V.M.
Solving the problem of stabilizing program deployment of an orbital tether system taking into account limitations on the rotary motion of the tip body
1 1., 1 1.
Determination of the optimal parameters and engine layout for a strike unmanned aerial vehicle
Zinenkov Y.V., Lukovnikov A.V., Agaverdyev S.V.
Planning a factorial experiment for testing a single-stage ultralow power turbine
Grigoryev V.A., Radko V.M., Kalabukhov D.S.
Feature of optimization of parameters of working process GTE with the free turbine at initial designing in the conditions of uncertainty
1 1., 1 1.
1 - 21 of 21 Items

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