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Verification of a transonic stage CFD model for assessing the erosion wear influence on the operation of the axial compressor
Blinov V.L., Zubkov I.S.
Comparative analysis of turbulence model influence in numerical simulation of an experimental radial compressor stage
Eremenko V.V., Mikhailov A.E., Mikhailova A.B., Goryukhin M.O., Krasnoperov D.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.
Influence of the stressed state of the surface layer on the endurance of gas turbine engine compressor blades
Sazonov M.B., Solovatskaya L.V.
Significance and directions of development of rotary piston area of research
Okorochkov V.V., Okorochkova V.M., Shafranov V.V.
Off-line long-life unservice close gas organic fuel-powered turbine
Arbekov A.N.
About the thermal protection of the oil cavities for designing gas turbine engines
Tryanov A.Y., Grishanov O.A., Vinogradov A.S.
Оptimization of gas turbine aircraft engine control throughout the engine service life
Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.
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.
Problem of multistage compressor optimization while designing perspective gas turbine engines
Shabliy L.S.
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.
Increasing the efficiency of rotary piston engines by the use of the diesel cycle
Okorochkov V.V., Okorochkova V.M., Ravodin A.I.
Experimental investigation of a small-sized centrifugal compressor for a closed-brayton cycle gas turbine power system
Arbekov A.N., Novitskiy B.B.
Aerodynamic improvement of GTE compressors by space profiling of blade vanes
Gerasimenko V.P., Shelkovsky M.Y.
Simulation of the distributed selection and supply of cooling air in gas-turb engine
Goryunov A.I., Goryunov I.M.
Peculiarities of computer modeling of the working process in small gas turbine engines
Kuz'michev V.S., Tkachenko A.Y., Ostapyuk Y.A.
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.
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.
Project of 30 000 h.p. power gas turbine
Zrelov V.A.
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.
Development of an exhaust air turbine engine
Yeliseev Y.S., Fedorchenco D.G., Tsibizov Y.I., Tyulkin D.D., Tkachenko A.Y.
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.
Thermodynamic calculation of a thermomechanical compressor
Blagin E.V., Dovgyallo A.I., Uglanov D.A., Dostovalova S.S.
Rotor blade compressor working process analysis
Dovgyallo A.I., Kolomin I.V.
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.
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.
Approaches to parametric models of blade machines formation
Shabliy L.S., Popov G.M., Kolmakova D.A.
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.
Hydrogenium saturation research for finishing pulsed electrochemical machining of titan alloy (BT9) TJ blades
Smirnov G.V.
Damping devices in the construction of compressor vanes of engines of the "NK" family
Frolov V.A., Belousov A.I.
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.
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.
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.
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.
Compressor blade erosion modeling
Gumerov A.V., Akmaletdinov R.G.
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.
Computation of tip clearance effect on characteristic of low pressure compressor of engine RD-33
Abdelwahid M.B., Fedorov R.M., Fedechkin K.S.
Laws of life dispersion and statistical estimation of life distribution boundaries as applied to aviation engine LPC disks
Kutyrev V.V., Teplova S.V.
1 - 38 of 38 Items

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