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Development of the criteria of analyzing the stress-strain state of gas turbine engine parts in the elastoplastic range
Bukaty A.S., Bukaty S.A.
Optimizing the process of changing spacecraft orbital parameters by using a spinning electrodynamic tether sytem
Lu H., Wang C., Zabolotnov Y.M.
Model of the turboprop engine reduction gear tooth harmonic spectral component
Sundukov A.E., Shakhmatov E.V.
Survey of the flight efficiency of a long-haul aircraft under uncertainty of tasks
Markiewicz P.
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.
Ultrasonic hardening of specimens made of ЭИ698 alloy optimal regimes choice using average integral residual stresses criterion
Pavlov V.F., Filatov A.P., Shadrin V.K., Chirkov A.V.
Improving the efficiency of aviation turbofan engines by using an intercooler and a recuperative heat exchanger
Omar H., Kuz'michev V.S., Tkachenko A.Y.
Optimal stabilization of small spacecraft angular motion in the process of deployment of an orbital tether system
Zabolotnov Y.M., Lobankov A.A.
Development of yield criteria for the calculation of forming high-textured anisotropic blanks
Grechnikov F.V., Yerisov Y.A.
Mathematical model of anisotropic elastic-plastic material
Grechnikov F.V., Yerisov Y.A.
Use of the dynamic programming method for solving tasks of GTE management optimization using the aircraft efficiency criteria
Tkachenko A.Y., Kuzmichev V.S.
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.
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.
Evaluation of thermochemical treatment influence on fatigue strength of specimens under normal and high temperatures
Pavlov V.F., Vakuljuk V.S., Afanasieva O.S., Bukatyi A.S.
Prediction of endurance limit of hardened parts with account of operational factors
Pavlov V.F., Kirpichev V.A., Kiselev P.E., Shvetsova A.A.
Forecasting an increment in the parts’ endurance limit due to surface hardening
Pavlov V.F., Filatov A.P., Semyonova O.Y., Sazanov V.V., Mikushev N.N.
Fatigue strength prediction of surface - hardened cylindrical specimens of different diameters
Kirpichev V.A., Pavlov V.F., Chirkov A.V., Ivanova A.V.
Backstepping synthesis of the height control system of an unmanned aerial vehicle
Akhramovich S.A., Barinov A.V., Malyshev V.V., Starkov A.V.
Criterion of optimization of slow fatigue crack growth in metals and alloys
Kol’tsoun Y.I., Molyavko D.P., Ignatovskiy A.D., Khibnik T.A.
Elastic-and-plastic problem for a thin plate with a non-yhrough crack cut for the case of localized strain according to rigid plastic flow schemes
Stepanov S.L.
Peculiarities of using hot-air balloons in tests of parachute systems
Kurinny S.M., Krivorotov M.M., Baranichenko E.A.
Deformation and fracture strength of single-crystal superalloys under static and cyclic loading
Semenov A.S., Getsov L.B., Semenov S.G., Grishchenko A.I.
Verifying models of mechatronic systems «man-centrifuge» for ground and space usage on the basis of set theory
Anshakov G.P., Akulov V.A., Balakin V.L.
Selection of reference specimens for assessing the efficiency of part surface nitriding
Sazanov V.V.
Dependence of the endurance limit on the character of residual stresses distribution in the surface layer of hardened parts
Kirpichyov V.A., Vakulyuk V.S., Bukaty A.S., Lunin V.V., Mikhalkina S.A.
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.
1 - 26 of 26 Items

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