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Two-dimentional axial rotor compressor off-design performance prediction model with the use of simulation methods and tools
Mikhailova A.B., Akhmedzyanov D.A., Akhmetov Y.M., Mikhailov A.Y.
Compressor blade erosion modeling
Gumerov A.V., Akmaletdinov R.G.
Methodology for thermal calculation of the heat exchanger for cooling the air at the intake of the aerospace plane engine compressor
Panchenko S.L., Gras’ko T.V.
Special aspects of numerical simulation of a two-stage axial-flow compressor with defective blades
Blinov V.L., Zubkov I.S., Iskortsev E.Y., Belyaev O.V., Plishkin P.I.
Influence of the stressed state of the surface layer on the endurance of gas turbine engine compressor blades
Sazonov M.B., Solovatskaya L.V.
Early detection of vibration behaviour of aircraft engine multistage axial compressor in pre-surge states during rig testing
Khorikov A.A., Danilkin S.Y., Mazikina T.I.
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.
Problem of multistage compressor optimization while designing perspective gas turbine engines
Shabliy L.S.
Thermodynamic calculation of a thermomechanical compressor
Blagin E.V., Dovgyallo A.I., Uglanov D.A., Dostovalova S.S.
Simulation of the distributed selection and supply of cooling air in gas-turb engine
Goryunov A.I., Goryunov I.M.
Application of the vacuum casting technology in the production of small-size gas turbine engine blade machines
Faramazyan A.M., Remchukov S.S., Demidyuk I.V.
Оptimization of gas turbine aircraft engine control throughout the engine service life
Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.
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.
Approaches to parametric models of blade machines formation
Shabliy L.S., Popov G.M., Kolmakova D.A.
Mathematical modeling of processes of compression and expansion in the piston pump with a gas damper
Shcherba V.E., Pavlyuchenko E.A., Kuzhbanov A.K.
Methods and the experiment of the parametric identification compressors and fans mathematical models of according to the results of the gas turbine engine development test
Kofman V.M.
Project of 30 000 h.p. power gas turbine
Zrelov V.A.
Damping devices in the construction of compressor vanes of engines of the "NK" family
Frolov V.A., Belousov A.I.
Increasing the efficiency of rotary piston engines by the use of the diesel cycle
Okorochkov V.V., Okorochkova V.M., Ravodin A.I.
Significance and directions of development of rotary piston area of research
Okorochkov V.V., Okorochkova V.M., Shafranov V.V.
Research of radial face contact seal tightness in the support of the aircraft engine compressor at various operational modes
Vinogradov A.S., Badykov R.R., Shpakov I.D.
Technological features of formation of the multifunctional nanostructured coverings of nitride of the titan for compressor shovels aviation GTD
Tarasenko Y.P., Tsareva I.N., Kocherov E.P., Vyazovskaya L.M.
Rotor blade compressor working process analysis
Dovgyallo A.I., Kolomin I.V.
Comparative analysis of facilities for the implementation of thermoplastic hardening blades of gas turbine engines and pumping units
Karpov A.V.
Peculiarities of computer modeling of the working process in small gas turbine engines
Kuz'michev V.S., Tkachenko A.Y., Ostapyuk Y.A.
Development of a mathematical model of winding made of non-impregnated aramid fibers for strength analysis of the combined fan case in GTE compressor blade separation
Krundaeva A.N., Shmotin Y.N., Tomilina T.V.
Simulating of Roots compressor
Belov G.O., Ermilov M.A., Kryuchkov A.N.
Nondestructive testing of the working compressor blades of the aviation engine
Nikitina N.E., Motova E.A., Tarasenko Y.P.
Special methodic of economics indexes determination of turbocompressor stations for central air supply of industrial factories
1 1., 1 1.
Hydrogenium saturation research for finishing pulsed electrochemical machining of titan alloy (BT9) TJ blades
Smirnov G.V.
Development of an exhaust air turbine engine
Yeliseev Y.S., Fedorchenco D.G., Tsibizov Y.I., Tyulkin D.D., Tkachenko A.Y.
Experimental investigation of a small-sized centrifugal compressor for a closed-brayton cycle gas turbine power system
Arbekov A.N., Novitskiy B.B.
Application of the artifical neyral networks theory methods for generalization and representation charachteristics of aviation gas turbine engines axial compressors
Grigoriev V.A., Kalabukhov D.S., Rad'ko V.M.
Optimization of aircraft seven stage compressor first stages parameters
Popov G.M., Matveev V.N., Baturin O.V., Kolmakova D.A.
Theoretical calculation approach of gas turbine engines compressor characteristic line
1 1.
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.
Research of the postoperational condition of the restored compressor shovels of GTD gas-transfer of the units which have fulfilled the appointed resource
Tarasenko Y.P., Tsareva I.N., Krivina L.A.
Study of uncertainty of measuring geometrical parameters of gas turbine engine compressor blade profiles
Pechenin V.A., Bolotov M.V., Ruzanov N.V., Yanyukina M.V.
Peculiarities of modeling the work process in a low-pressure compressor of a gas turbine plant
Matveev V.N., Popov G.M., Goryachkin E.S., Smirnova Y.D.
Computation of tip clearance effect on characteristic of low pressure compressor of engine RD-33
Abdelwahid M.B., Fedorov R.M., Fedechkin K.S.
Investigation of effects of multistage compressor final stage blading shape on compressor performance and flow pattern
Popov G.M., Krivcov A.V., Kolmakova D.A.
Probabilistic estimate of compressor blades durability to foreign object damage
1 1., 1 1.
Vortex wind power plant
Biryuk V.V., Krasnorutskiy A.S.
The possibility of ultrasonic testing of compressor blades after exploitation and repair
Motova E.A., Nikitina N.Y.
Development and analysis of screw restrictor hydraulic characteristics in the air bleed valve control unit of a gas turbine engine
Gimadiev A.G., Makaryants G.M., Blyumin K.V., Dudnichenko I.M.
Structural and acoustic anisotropy of turbocompressor blade material
Tarasenko Y.P., Krivina L.A., Motova E.A., Nikitina N.Y.
Off-line long-life unservice close gas organic fuel-powered turbine
Arbekov A.N.
Aerodynamic improvement of GTE compressors by space profiling of blade vanes
Gerasimenko V.P., Shelkovsky M.Y.
About the thermal protection of the oil cavities for designing gas turbine engines
Tryanov A.Y., Grishanov O.A., Vinogradov A.S.
The nature of change in the residual stress-strain state of dovetail lock joints, taking into account nonlinear strains
Zhernakov V.S., Mardimasova T.N., Koneva K.V.
Theory of gas turbine engine optimal gas generator
Grigoriev A.V., Kosmatov A.A., Rudakov О.A., Solovieva A.V.
The use of mathematical optimization means to increase the efficiency of a seven-stage axial flow compressor
Baturin O.V., Popov G.M., Gorachkin E.S., Novikova Y.D.
Post-operation state and extension of service life of compressor blades of the gas-turbine power plant GTE-45-3
Tarasenko Y.P., Berdnik O.B., Tsareva I.N.
Improving the high pressure compressor efficiency by optimizing the stator blades angles
Popov G.M.
Method of calculating GTE gas-thermodynamic parameters with blade row description of an axial multistage compressor
Boyko L.G., Karpenko E.L., Akhtemenko U.F.
Rotor-vane compressor with working chambers contactless condensation optimizations variants
Kolomin I.V., Dovgjallo A.I., Galperin R.N., Gulyaev L.Y., Logashkin A.P.
1 - 56 of 56 Items

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