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Peculiarities of using hot-air balloons in tests of parachute systems
Kurinny S.M., Krivorotov M.M., Baranichenko E.A.
Check and prediction of gas-turbine engine’s technical state
Zotin N.A.
Processing of experimental data by the method of the least squares
Ovchinnikov A.V., Krasnochub E.K., Bronstein V.M.
Determination of the optimal parameters and engine layout for a strike unmanned aerial vehicle
Zinenkov Y.V., Lukovnikov A.V., Agaverdyev S.V.
Criterion assessment of the possibility to prolong the service life limit of the helicopter tail drive shaft
Mashoshin O.F., Semenikhin R.L.
Development of yield criteria for the calculation of forming high-textured anisotropic blanks
Grechnikov F.V., Yerisov Y.A.
Use of the mathematical tool of hypervector ranging for selection energy-power plant of flight vehicles
Safronov V.V., Zhebrakov A.S.
The effect of heat recovery on the optimal values of helicopter turboshaft engine parameters
Omar H.H., Kuz'michev V.S., Zagrebelnyi A.O., Grigoriev V.A.
Mathematical models for evaluating the energy efficiency of ultralow power turbine drives
Kalabuhov D.S., Grigoryev V.A., Rad’ko V.M.
Use of the dynamic programming method for solving tasks of GTE management optimization using the aircraft efficiency criteria
Tkachenko A.Y., Kuzmichev V.S.
Methods and models of autonomous control over Earth remote sensing spacecraft survivability
Akhmetov R.N.
Technique of conclusion the direct-flow detonation pulsing engine design to the leader position
Safronov V.V., Porshnev V.A., Zhebrakov A.S.
Mathematical model of anisotropic elastic-plastic material
Grechnikov F.V., Yerisov Y.A.
Peculiarities of heat transfer in thermoacoustic converters
Dovgyallo A.I., Nekrasova S.O.
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.
Methodology of optimization of parameter of matching the combustion chamber and turbine joint operation
Grigoriev A.V., Golubchikov P.P., Ilushin M.Y., Rudakov O.A., Solovieva A.V.
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.
Energy optimality criteria
Danilin A.I.
Choosing the place for the installation of navigation system aerials on the ERS spacecraft body
Akhmetov R.N., Kurenkov V.I., Stratilatov N.R., Shilov L.B., Gordeev A.I.
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.
Estimation of static strength of sections of the linear pipeline portion with a colony of corrosion fine cracks
Subbotin V.A., Scherbo I.V., Kholodkov S.A., Giorbelidze M.G.
Mathematical models of optimal investment control in fixed assets
Pavlov O.V., Moshkova T.A.
Shaping technologies for manufacturing noise insulation casings of turbojet engines
Molod M.V., Maksimenkov V.I., Fedoseev V.I.
Problems of ultralow power turbine design in a turbine drive system
Kalabuhov D.S., Grigoryev V.A., Rad’ko V.M.
Processing of experimental data by the method of the least squares
1 1., 1 1., 1 1.
Methodological and analytical support for the creation and maintenance of aerospace industry technological development strategic programs
Gaponenko O.V.
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.
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.
1 - 28 of 28 Items

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