Issue
Title
Authors
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.
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.
Vortex wind power plant
Biryuk V.V., Krasnorutskiy A.S.
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.
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.
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.
Aerodynamic improvement of GTE compressors by space profiling of blade vanes
Gerasimenko V.P., Shelkovsky M.Y.
Thermodynamic calculation of a thermomechanical compressor
Blagin E.V., Dovgyallo A.I., Uglanov D.A., Dostovalova S.S.
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.
Experimental investigation of a small-sized centrifugal compressor for a closed-brayton cycle gas turbine power system
Arbekov A.N., Novitskiy B.B.
Structural and acoustic anisotropy of turbocompressor blade material
Tarasenko Y.P., Krivina L.A., 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.
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.
Off-line long-life unservice close gas organic fuel-powered turbine
Arbekov A.N.
Compressor blade erosion modeling
Gumerov A.V., Akmaletdinov R.G.
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.
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.
Nondestructive testing of the working compressor blades of the aviation engine
Nikitina N.E., Motova E.A., Tarasenko Y.P.
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.
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.
Significance and directions of development of rotary piston area of research
Okorochkov V.V., Okorochkova V.M., Shafranov V.V.
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.
Rotor blade compressor working process analysis
Dovgyallo A.I., Kolomin I.V.
Computation of tip clearance effect on characteristic of low pressure compressor of engine RD-33
Abdelwahid M.B., Fedorov R.M., Fedechkin K.S.
Hydrogenium saturation research for finishing pulsed electrochemical machining of titan alloy (BT9) TJ blades
Smirnov G.V.
Peculiarities of computer modeling of the working process in small gas turbine engines
Kuz'michev V.S., Tkachenko A.Y., Ostapyuk Y.A.
Improving the high pressure compressor efficiency by optimizing the stator blades angles
Popov G.M.
Problem of multistage compressor optimization while designing perspective gas turbine engines
Shabliy L.S.
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.
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.
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.
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.
About the thermal protection of the oil cavities for designing gas turbine engines
Tryanov A.Y., Grishanov O.A., Vinogradov A.S.
Approaches to parametric models of blade machines formation
Shabliy L.S., Popov G.M., Kolmakova D.A.
Optimization of aircraft seven stage compressor first stages parameters
Popov G.M., Matveev V.N., Baturin O.V., Kolmakova D.A.
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.
Theory of gas turbine engine optimal gas generator
Grigoriev A.V., Kosmatov A.A., Rudakov О.A., Solovieva A.V.
Simulation of the distributed selection and supply of cooling air in gas-turb engine
Goryunov A.I., Goryunov I.M.
Influence of the stressed state of the surface layer on the endurance of gas turbine engine compressor blades
Sazonov M.B., Solovatskaya L.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.
Increasing the efficiency of rotary piston engines by the use of the diesel cycle
Okorochkov V.V., Okorochkova V.M., Ravodin A.I.
Development of an exhaust air turbine engine
Yeliseev Y.S., Fedorchenco D.G., Tsibizov Y.I., Tyulkin D.D., Tkachenko A.Y.
Damping devices in the construction of compressor vanes of engines of the "NK" family
Frolov V.A., Belousov A.I.
Special methodic of economics indexes determination of turbocompressor stations for central air supply of industrial factories
1 1., 1 1.
Comparative analysis of facilities for the implementation of thermoplastic hardening blades of gas turbine engines and pumping units
Karpov A.V.
Theoretical calculation approach of gas turbine engines compressor characteristic line
1 1.
Probabilistic estimate of compressor blades durability to foreign object damage
1 1., 1 1.
The possibility of ultrasonic testing of compressor blades after exploitation and repair
Motova E.A., Nikitina N.Y.
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.
Simulating of Roots compressor
Belov G.O., Ermilov M.A., Kryuchkov A.N.
Project of 30 000 h.p. power gas turbine
Zrelov V.A.
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.
1 - 52 of 52 Items

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