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Limit values of the Brayton cycle with the use of reduced fuel characteristics
Mikheenkov E.L., Nekrasova S.O.
Features of dynamic processes in the “indentor – coating” system during tests on a tribometer
Kolesnikov I.V., Koropets P.A., Manturov D.S., Shakhmatov Y.V.
The problems of creating a propulsion system of a new generation supersonic passenger aircraft (review)
Alendar A.D., Lanshin A.I., Evstigneev A.A., Yakubovsky K.Y., Siluyanova M.V.
Heat engine cycle limitations imposed by fuel properties
Mikheyenkov E.L.
Relation between characyeristics of low-cycle and high-cycle fatigue of threaded parts and residual stresses
Zlobin A.S.
Method of reduced fuel characteristics and parameters of the operating cycles of heat engines
Anastaseev V.V., Belozertsev S.V., Mikheenkov E.L., Nekrasova S.O.
The analysis of real thermodynamic cycle of bypass engine with mixing
Medvedev V.V.
Product life cycle in the aspect of postulates of logistics and labour object theory
Sosnina T.N.
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.
Efficiency of complex cycles of gas turbine units with air bleed for the cooling of intermediate combustion chambers
Ivanov V.A.
Mathematical model for calculating the mass of a heat exchanger in problems of optimizing the parameters of the working process of aircraft gas turbine engines
Kuz'michev V.S., Omar H., Tkachenko A.Y., Bobrik A.A.
Efficiency of complex cycles of a gas turbine unit with varying degrees of heating in the first and second stages
Ivanov V.A.
Study of processes production scheduling in multiproduct manufactures
Larin S.N., Timirzyanov V.V.
Progressive thermodynamic cycle of internal combustion engine based on сrank a rod the mechanism with dual kinematic communications
Grabovskiy A.A.
Process of autoreengineering of entreprise common information space
Ivashchenko A.V.
Preliminary study of principles of effective efficiency change of turboshaft engines of various schemes with heat recovery and intermediate cooling of working medium
Sokolov M.A., Kuzmichev V.S., Kulagin V.V., Krupenich I.N., Tkachenko A.Y.
Methods of evaluating low-cycle fatigue of gas turbine engine parts exemplified by a high-pressure turbine cover plate
Kocherova E.E.
Study of cycle life of a material in conditions of low-cycle fatigue and long-term strength
Bukatyi S.A., Okrugin A.A.
Experimental verification of the specified characteristics of a solar battery at the stages of production and ground operation
Shuplyak Y.P., Sorokoletov V.I.
Fatigue resistange of turbine blade roots under combined stress
Gladkov A.V., Solyannikov V.A., Zhuzhukin A.I.
Increasing the reliability of aircraft components by regulating technological residual stress
Kirpitchyov V.A., Vakulyuk V.S., Tchirkov A.V.
Estimation of parameters of a pulse detonation engine (РDЕ)
Anakin A.T., Tsybizov Y.I.
Harmonic model of thermodynamic cycle in thermoacoustic engine regenerator
Zynovyev E.A., Dovgyallo A.I., Vorotnikov G.V.
Evaluation of low cycle fatigue based on the use of Coffin-Manson dependence under zero-to-“soft” loading cycle
Pavlov V.F., Kirpichyov V.A., Kocherova E.E., Zlobin A.S.
Experimental investigation of a small-sized centrifugal compressor for a closed-brayton cycle gas turbine power system
Arbekov A.N., Novitskiy B.B.
Improving the efficiency of gas turbines by regenerating heat
Kulagin V.V., Sokolov M.A.
Multi-scale complex failure analysis of aero engine compressor disks
Tumanov N.V., Porter A.M., Lavrentyeva M.A., Cherkasova S.A., Vorobyova N.A., Lyoshin D.P.
The community of the ideal and complex cycles of the gas-turbine installations
Ivanov V.A.
To a question of forcing up of thermal stirlings macine
Belozertcev V.N.
Improvement of gas turbine engines due to isothermal expansion in the turbine
Muraeva M.A., Gorjunov I.M.
Development of a prototype of a multi-loop closedbrayton cycle gas turbine power system
Arbekov A.N., Novitskiy B.B.
Cycle air heating system of gas pumping unit NEVA-25NK
1 1., 1 1., 1 1., 1 1.
Mathematical model of surface layer formation during hydroabrasive jet machining
Meshcheryakov A.V., Shulepov A.P.
Cycle parameters of an internal combustion spark-ignition gas piston engine with an electronic control system
Shishkov V.A.
Optimization methods pilotage aircraft in take-off and approach cycle for decrease square his sound track
Zamtfort B.S., Medvedev Y.V.
Features of designing gas turbine of complex cycle GT24
1 1.
Procedure rules of press forging business process development and coordination
Khaimovitch I.N., Khaimovitch A.I.
Analysis of basic concepts of advanced engines for supersonic civil aircraft on the basis of foreign designers’ experience
Alendar A.D., Grunin A.N., Siluyanova M.V.
Education organization in common information sphere given about product
Prodanov M.Y.
Simulation of wire manufacturing production cycle
Haymovich I.N., Skripachyov D.G., Kolesnikova S.Y.
Kinetic equation of stable growth for low cycle fatigue cracks
Tumanov N.V.
Ontology description languages for high-tech fields of applied engineering
Burakova E.E., Borgest N.M., Korovin M.D.
Way of increase in efficiency of cycle gas turbine units
1 1.
Mathematical modeling of dynamic processes in a hydraulic drive with a discrete regulator of liquid flow
Shakhmatov Y.V., Gimadiev A.G., Sverbilov V.Y., Sinyakov A.F.
Study of mechanisms of low cycle fatigue crack propagation in aero engine disks under operating conditions and disk residual life estimation
Tumanov N.V., Cherkasova S.A., Lavrentyeva M.A., Vorobyeva N.A.
Dependence of energy characteristics of Stirling gas refrigerating machines on external and internal parametric values
Belozertsev V.N.
Conception of cycle life additivity and its application for determining the resource of aero engine disks
Tumanov N.V., Lavrentyeva M.A.
The interactive system for collecting data of technical condition of aircraft components
Blagorazumov A.K., Kirpichev I.G.
The integrated information model architecture for working out, manufacture and operation GTE together with its system of automatic control, the control and diagnostics
Kulikov G.G., Rizvanov K.A., Denisova S.S.
Applying the possibilities of Microsoft Excel for solving problems of fuel burning thermodynamics
Mikheenkov E.L., Nekrasova S.O., Ramzaeva E.A.
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.
Theory and calculation of parameters of the detonation engine thermodynamical cycle
Grigoriev A.V., Mitrofanov V.A., Rudakov O.A., Solovieva A.V.
Simulation of operaiting cycle by Petry nets
Zelenskiy V.A., Konnov V.P., Schodro A.I.
Evaluation of internal combustion engine cycle work using an ionic current sensor
Ivashin P.V., Ramazanov M.P., Tverdokhlebov A.Y., Shaikin A.P., Yasnikov I.S.
Modeling stable growth of fatigue cracks in aero engine turbine discs under simple and complex loading cycles
Tumanov N.V., Lavrentyeva M.A., Cherkasova S.A., Servetnik A.N.
1 - 55 of 55 Items

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