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Vol 22, No 1 (2023)

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.

(Rus)

Vol 22, No 4 (2023)

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.

(Rus)

Vol 21, No 4 (2022)

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.

(Rus)

Vol 18, No 1 (2019)

Influence of the stressed state of the surface layer on the endurance of gas turbine engine compressor blades

Sazonov M.B., Solovatskaya L.V.

(Rus)

Vol 13, No 5-3 (2014): Special Issue

Significance and directions of development of rotary piston area of research

Okorochkov V.V., Okorochkova V.M., Shafranov V.V.

(Rus)

Vol 11, No 3-2 (2012): Special Issue

Off-line long-life unservice close gas organic fuel-powered turbine

Arbekov A.N.

(Rus)

Vol 8, No 3-1 (2009): Special Issue

About the thermal protection of the oil cavities for designing gas turbine engines

Tryanov A.Y., Grishanov O.A., Vinogradov A.S.

(Rus)

Vol 17, No 4 (2018)

Оptimization of gas turbine aircraft engine control throughout the engine service life

Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.

(Rus)

Vol 13, No 5-2 (2014): Special Issue

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.

(Rus)

Vol 11, No 3-2 (2012): Special Issue

Problem of multistage compressor optimization while designing perspective gas turbine engines

Shabliy L.S.

(Rus)

Vol 8, No 3-1 (2009): Special Issue

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.

(Rus)

Vol 15, No 4 (2016)

Increasing the efficiency of rotary piston engines by the use of the diesel cycle

Okorochkov V.V., Okorochkova V.M., Ravodin A.I.

(Rus)

Vol 13, No 5-2 (2014): Special Issue

Experimental investigation of a small-sized centrifugal compressor for a closed-brayton cycle gas turbine power system

Arbekov A.N., Novitskiy B.B.

(Rus)

Vol 12, No 3-2 (2013): Vestnik SSAU

Aerodynamic improvement of GTE compressors by space profiling of blade vanes

Gerasimenko V.P., Shelkovsky M.Y.

(Rus)

Vol 8, No 3-1 (2009): Special Issue

Simulation of the distributed selection and supply of cooling air in gas-turb engine

Goryunov A.I., Goryunov I.M.

(Rus)

Vol 15, No 4 (2016)

Peculiarities of computer modeling of the working process in small gas turbine engines

Kuz'michev V.S., Tkachenko A.Y., Ostapyuk Y.A.

(Rus)

Vol 13, No 5-1 (2014): Special Issue

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.

(Rus)

Vol 12, No 3-2 (2013): Vestnik SSAU

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.

(Rus)

Vol 8, No 3-1 (2009): Special Issue

Project of 30 000 h.p. power gas turbine

Zrelov V.A.

(Rus)

Vol 20, No 4 (2021)

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.

(Rus)

Vol 15, No 4 (2016)

Development of an exhaust air turbine engine

Yeliseev Y.S., Fedorchenco D.G., Tsibizov Y.I., Tyulkin D.D., Tkachenko A.Y.

(Rus)

Vol 11, No 3-3 (2012): Special Issue

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.

(Rus)

Vol 12, No 3-2 (2013): Vestnik SSAU

Thermodynamic calculation of a thermomechanical compressor

Blagin E.V., Dovgyallo A.I., Uglanov D.A., Dostovalova S.S.

(Rus)

Vol 8, No 2 (2009)

Rotor blade compressor working process analysis

Dovgyallo A.I., Kolomin I.V.

(Rus)

Vol 20, No 3 (2021)

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.

(Rus)

Vol 14, No 3-2 (2015): Special Issue

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.

(Rus)

Vol 11, No 3-3 (2012): Special Issue

Approaches to parametric models of blade machines formation

Shabliy L.S., Popov G.M., Kolmakova D.A.

(Rus)

Vol 10, No 3-1 (2011): Special Issue

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.

(Rus)

Vol 7, No 3 (2008): Special Issue

Hydrogenium saturation research for finishing pulsed electrochemical machining of titan alloy (BT9) TJ blades

Smirnov G.V.

(Rus)

Vol 10, No 3-3 (2011): Special Issue

Damping devices in the construction of compressor vanes of engines of the "NK" family

Frolov V.A., Belousov A.I.

(Rus)

Vol 14, No 3-1 (2015): Special Issue

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.

(Rus)

Vol 11, No 3-3 (2012): Special Issue

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.

(Rus)

Vol 10, No 3-1 (2011): Special Issue

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.

(Rus)

Vol 12, No 3-1 (2013): Vestnik SSAU

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.

(Rus)

Vol 10, No 3-2 (2011): Special Issue

Compressor blade erosion modeling

Gumerov A.V., Akmaletdinov R.G.

(Rus)

Vol 10, No 5 (2011)

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.

(Rus)

Vol 11, No 3-3 (2012): Special Issue

Computation of tip clearance effect on characteristic of low pressure compressor of engine RD-33

Abdelwahid M.B., Fedorov R.M., Fedechkin K.S.

(Rus)

Vol 8, No 3-1 (2009): Special Issue

Laws of life dispersion and statistical estimation of life distribution boundaries as applied to aviation engine LPC disks

Kutyrev V.V., Teplova S.V.

(Rus)

1 - 38 of 38 Items

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