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Compressor blade erosion modeling

Gumerov A.V., Akmaletdinov R.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 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 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 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)

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)

Problem of multistage compressor optimization while designing perspective gas turbine engines

Shabliy L.S.

(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)

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

Goryunov A.I., Goryunov I.M.

(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 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 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)

Approaches to parametric models of blade machines formation

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

(Rus)

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.

(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)

Project of 30 000 h.p. power gas turbine

Zrelov V.A.

(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 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 5-3 (2014): Special Issue

Significance and directions of development of rotary piston area of research

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

(Rus)

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.

(Rus)

Vol 11, No 3-1 (2012): Special Issue

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.

(Rus)

Vol 8, No 2 (2009)

Rotor blade compressor working process analysis

Dovgyallo A.I., Kolomin I.V.

(Rus)

Comparative analysis of facilities for the implementation of thermoplastic hardening blades of gas turbine engines and pumping units

Karpov A.V.

(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 5-2 (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)

Simulating of Roots compressor

Belov G.O., Ermilov M.A., Kryuchkov A.N.

(Rus)

Vol 11, No 3-1 (2012): Special Issue

Nondestructive testing of the working compressor blades of the aviation engine

Nikitina N.E., Motova E.A., Tarasenko Y.P.

(Rus)

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

Special methodic of economics indexes determination of turbocompressor stations for central air supply of industrial factories

1 1., 1 1.

(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 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 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)

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 11, No 5-1 (2012): Special Issue

Optimization of aircraft seven stage compressor first stages parameters

Popov G.M., Matveev V.N., Baturin O.V., Kolmakova D.A.

(Rus)

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

Theoretical calculation approach of gas turbine engines compressor characteristic line

1 1.

(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)

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.

(Rus)

Vol 15, No 2 (2016)

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.

(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)

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 11, No 5-1 (2012): Special Issue

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.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

Probabilistic estimate of compressor blades durability to foreign object damage

1 1., 1 1.

(Rus)

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

Vortex wind power plant

Biryuk V.V., Krasnorutskiy A.S.

(Rus)

The possibility of ultrasonic testing of compressor blades after exploitation and repair

Motova E.A., Nikitina N.Y.

(Rus)

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

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.

(Rus)

Vol 13, No 4 (2014)

Structural and acoustic anisotropy of turbocompressor blade material

Tarasenko Y.P., Krivina L.A., Motova E.A., Nikitina N.Y.

(Rus)

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

Arbekov A.N.

(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)

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

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

(Rus)

Vol 21, No 1 (2022)

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.

(Rus)

Vol 18, No 2 (2019)

Theory of gas turbine engine optimal gas generator

Grigoriev A.V., Kosmatov A.A., Rudakov О.A., Solovieva A.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 13, No 4 (2014)

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.

(Rus)

Improving the high pressure compressor efficiency by optimizing the stator blades angles

Popov G.M.

(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)