Issue
Title
Authors
Formation of a method of choosing rational values of ultralow power turbine parameters in a turbine drive system
Kalabuhov D.S., Grigoryev V.A., Rad’ko V.M.
Discrete phase converters moving elements rotating units power units
Danilin A.I., Grechishnikov V.M.
Effect of radial location of nozzles on width on performance of pre-swirl systems
Didenko R.A., Karelin D.V., Ievlev D.G., Lebedev V.V.
Development of methods of designing modern gas turbines
Inozemtsev A.A., Khairulin V.T., Tikhonov A.S., Samokhvalov N.Y.
Defects of shrouded blade platforms of high-temperature gas turbines
Belousov A.I., Nazdrachyov S.V.
Evaluating the possibility of using low-temperature thermal energy in liquefied natural gas complexes
Dovgjallo A.I., Sarmin D.V., Uglanov D.A., Shimanov A.A.
Design of the gas turbine engine rotor wheel with ceramic blades
Sapronov D.V., Reznik S.V.
Optimization of the workflow of multistage axial turbines with platforms
Matveev V.N., Baturin O.V., Popov G.M., Goryachkin E.S.
Off-line long-life unservice close gas organic fuel-powered turbine
Arbekov A.N.
Simulation of aircraft multistage axial turbine working processes taking into account over-shroud leakage flows and blading inflows
Baturin O.V., Popov G.M., Kolmakova D.A.
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.
Validation of CFD-models of gas turbine engine uncooled turbines
Matveev V.N., Popov G.M., Goryachkin E.S., Smirnova Y.D.
Development of turbopump unit design for hydrogen liquid-propellant rocket engines without generators developed at the design bureau of chemical automation
Dmitrenko A.I., Ivanov A.V., Rachuk V.S.
Possibility of using a bi-directional impulse turbine in a thermo-acoustic engine
Dovgjallo A.I., Shimanov A.A.
Combined calculation of gas generators of small GTE in package ANSYS CFX
Matveev S.G., Orlov M.Y., Matveev S.S., Zinkovskii V.S., Krivtsov A.V.
Problems of ultralow power turbine design in a turbine drive system
Kalabuhov D.S., Grigoryev V.A., Rad’ko V.M.
Computational research of multistage turbine flow taking into account flow spatial structure and associated volumes
Baturin O.V., Senchev M.N., Dzhibilov P.T.
Design of bimetallic impeller for gas turbine
Magerramova L.A.
Experimental research of heat exchange in a plane channel using the regular thermal regime mrthod with different Biot numbers
Kolesova E.G., Veretennikov S.V., Zhornik M.N.
Criteria of discrete phase control of blade working condition and their feasibility in systems of turbine driven set automatic control
Danilin A.I., Tchernyavsky A.Z.
Method of coordinating joint operation of air starter and auxiliary power unit and determining the gas turbine engine starting time
Popov G.M., Baturin O.V., Novikova Y.D., Zubanov V.M., Volkov A.A., Korneeva A.I.
Volume and mass mathematical models of single-stage centripetal ultralow power turbines
Grigoriev V.A., Kalabukhov D.S., Rad'ko V.M.
Vortex effect and intensification of heat and mass transfer in cell energy technology
Piralishvily S.A., Veretennikov S.V.
Gas-turbine unit development experience for rotors wedging correction
Kozlyakova I.S., Krupin V.P., Potkin A.N., Fadeev V.A.
Effect of cavity width on performance of pre-swirl systems
Didenko R.A., Karelin D.V., Ievlev D.G., Lebedev V.V., Belousova E.V.
Evaluation of turbine rotor blade life taking into account static and thermal cyclic loading
Badamshin I.K.
Methods of evaluating low-cycle fatigue of gas turbine engine parts exemplified by a high-pressure turbine cover plate
Kocherova E.E.
About the thermal protection of the oil cavities for designing gas turbine engines
Tryanov A.Y., Grishanov O.A., Vinogradov A.S.
Peculiarities of computer modeling of the working process in small gas turbine engines
Kuz'michev V.S., Tkachenko A.Y., Ostapyuk Y.A.
Simulation of the distributed selection and supply of cooling air in gas-turb engine
Goryunov A.I., Goryunov I.M.
The concept of matching the joint operation of the combustion chamber, the compressor and the turbine
Grigoriev A.V., Golubchikov P.P., YIlushin M.Y., Rudakov O.A., Solovieva A.V.
The devices for the diagnosis and control of turbine blades deformative condition during operation
Danilin A.I., Chernyavskiy A.G., Kapustin A.S.
Method for optimizing mass and size characteristics of a high-pressure turbine disk
Siluyanova M.V., Grunin A.N., Alendar A.D., Kandaurov S.K.
Calculated study of tangential inclination of nozzle vanes influence on gas-dynamic efficiency of axial turbine stage
Baturin O.V., Matveev V.N.
Proposals for improving the efficiency and service life of the turbines of turbo-pump assemblies in liquid-propellant rocket engines by using double-sided crest-type radial labyrinth seals
Levochkin P.S., Chvanov V.K., Vasiliev V.S., Timushev S.F.
Optimization characteristics of rotor-support system from NK-14ST free power turbine with consider statics and dynamics propertys
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.
Formation of a structural calculated mesh the passage blade of the axial turbine in program GAMBIT
Baturin N.V., Baturin O.V., Matveev V.N.
Development of an exhaust air turbine engine
Yeliseev Y.S., Fedorchenco D.G., Tsibizov Y.I., Tyulkin D.D., Tkachenko A.Y.
Project of 30 000 h.p. power gas turbine
Zrelov V.A.
Influence of the loading parameter on the efficiency ofa three-stage turbine of turbojet bypass engine
1 1., 1 1.
The calculated study of fluid structure in a hub an axial aviation turbine
1 1., 1 1.
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.
Blading of radial-axial turbine wheel using Bezier curve
Baturin O.V.
Determination of a rational combination of the radial turbine basic parameters with an allowance for strength, technological and other constraints
Baturin O.V., Shabliy L.S.
1 - 45 of 45 Items

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