Search

Development of a virtual prototype of gasturbine engine at the stage of conceptual thermogasdynamic designusing the CAE-system «ASTRA»

Tkachenko A.Y., Krupenich I.N.

(Rus)

Gas turbine engine simulation strategy in CAE systems

Krivcov A.V.

(Rus)

Quasi one-dimensional model and calculation of processes in gas turbineengine combustion chambers given the heterogeneity of the combustible mixture, changes in mass, composition, temperature and stirring efficiency of the working body

Numerical modeling on dynamic process of injection in supersonic part of the nozzle

Yakovchuk M.S.

(Rus)

Vol 11, No 2 (2012)

Simulator, algorithm and software for the computation of differential gas circuits frequency response

Igonin A.A., Gimadiev A.G.

(Rus)

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

Didenko A.A., Sokolov A.B.

(Rus)

Prospects for the forcing of gas turbine and steam power plants

Pavlova A.A.

(Rus)

Vol 10, No 1 (2011)

Definition of directions of developing methods, technical decisions and means of decreasing the technogenic influence on the environment for the omplementation on board of space launch vehicles

Shatrov Y.T., Baranov D.A., Trushlyakov V.I., Kudentsov V.Y.

(Rus)

A separator skidding in the cylindrical roller bearing between shafts of the gas turbine engine

1 1., 1 1., 1 1.

(Rus)

Features of designing gas turbine of complex cycle GT24

1 1.

(Rus)

CFD-based modeling of oil ang gas journal bearings using commercial software packages

Pugachev A.O., Ravikovich Y.A., Ermilov Y.I., Kholobtsev D.P., Matushkin A.A.

(Rus)

System of pressurization of the fuel tank of a launch vehicle using the heat of generator gas

Biryuk V.V., Smorodin A.V., Shepelev A.I., Onoprienko D.A.

(Rus)

Vol 20, No 1 (2021)

Mathematical model of turbofan engine weight estimation taking into account the engine configuration and size

Avdeev S.V.

(Rus)

Vol 18, No 3 (2019)

Design of experiments for verification of computational life prediction methods

Samsonova O.V., Fetisov K.V., Karpman I.V., Burtseva I.V.

(Rus)

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

Features of start-up the engine of internal combustion with spark ignition on gas fuel

Shishkov V.A.

(Rus)

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

Experiment-calculated research of the influence of the shot-peening strengthening upon the low-cycle fatigue of the gas turbine parts with the stress concentrator

Porter A.M., Bukaty S.A., Leshin D.P., Bukaty A.S.

(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 17, No 3 (2018)

Analysis of schemes of correction of dynamic characteristics of acoustic probes for measuring pressure pulsations in a gas turbine engine

Gimadiev A.G., Bystrov N.D., Dyagileva E.S.

(Rus)

Vol 16, No 4 (2017)

The use of gas-dynamic flame stabilization in afterburner combustion chambers of aircraft gas turbine engines

Kolesnikov A.S., Pakhol'chenko A.A.

(Rus)

Vol 15, No 4 (2016)

Morphological characteristics of the intermetallic phase of heat resisting nickel alloys

Kirikov S.V., Perevezentsev V.N., Tarasenko Y.P.

(Rus)

Vol 15, No 3 (2016)

Laser powder weld reconditioning of gas turbine engine blades

Korsmik R.S., Turichin G.A., Klimova-Korsmik O.G., Zemlyakov E.V., Babkin K.D.

(Rus)

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

Application of numerical simulation systems for the research of the blade casting process in blank production

Smelov V.G., Vdovin R.A., Agapovichev A.V.

(Rus)

Vol 10, No 5 (2011)

Simulation of aerodynamic structure of the flow in the combustion chamber of a small-size gas turbine engine with the help of CAE–systems

Matveev S.G., Orlov M.Y., Abrashkin V.Y., Zubrilin I.A., Matveev S.S.

(Rus)

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

Development of a prototype of a multi-loop closedbrayton cycle gas turbine power system

Arbekov A.N., Novitskiy B.B.

(Rus)

Vol 11, No 4 (2012)

Stabilization of a pilot-operated gas pressure control valve by placing a throttle at the inlet

Stadnik D.M., Sverbilov V.Y., Makaryants G.M., Makaryants M.V.

(Rus)

Working conditions analysis of rotor supports bearings in aviation gas turbine engines and energetic units structure

Zrelov V.A., Makarchuk V.V., Prodanov M.E., Sudarev A.A.

(Rus)

Problem of multistage compressor optimization while designing perspective gas turbine engines

Shabliy L.S.

(Rus)

The use of gas turbines in small-scale installations of synthetic fuels

Filipchenko S.A., Faridonov R.R., Gushchina T.V.

(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)

Generation of control programes for disposable unmanned aircraft vehicle propulsion system by means of dynamic characteristic

Mikhailov A.Y., Akhmedzyanov D.A., Akhmetov Y.M., Mikhailova A.B.

(Rus)

Vol 9, No 4 (2010)

Variations in free cross-sectional areas of the phases of double-phase flows under changes of gaseous phase rate of flow

Levkin Y.S.

(Rus)

Designing and experimental research of hybrid gas bearings for heavy multibasic rotor of gas turbine

1 1.

(Rus)

Way of increase in efficiency of cycle gas turbine units

1 1.

(Rus)

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

Pressure-gain combustion and its potential for gas turbine engine enhancement

Lutoschkin E.V., Rose M.G., Staudacher S.

(Rus)

Test case of 3d unsteady swirling flows modeling using commercial and in-house codes

Nazukin V.A., Avgustinovich V.G., Thornber B., Aguado Lopez P., Tsatiashvili V.V., Koromyslov E.V.

(Rus)

Estimation of parameters of a pulse detonation engine (РDЕ)

Anakin A.T., Tsybizov Y.I.

(Rus)

Vol 19, No 4 (2020)

Сalculation of characteristics of atomization of liquid supplied at an angle to the flow direction and justification of adjusting the angle of the nozzle inclination relative to the gas flow

Teslya D.N., Mityaev S.V., Drobyshev P.A.

(Rus)

Vol 18, No 3 (2019)

Сalculated analysis of the influence of operation and design factors on the parameters of oxygen-hydrogen low-thrust rocket engines

Ryzhkov V.V., Morozov I.I.

(Rus)

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

Possibility of use of passing gases in gasturbine engines created within the limits of conversion

Rosljakov A.D., Kocherov E.P., Tsibizov J.I.

(Rus)

Vol 18, No 2 (2019)

Ensuring permissible level of gas turbine dynamic loading in operation by means of standard engine control devices

Chervonyuk V.V., Korovin B.B.

(Rus)

Vol 18, No 1 (2019)

Research of the operability of an air-fuel lubrication and cooling system of gas turbine engine rotor bearings

Klimov V.N., Dud’ev D.Y., Sigaylo V.Y., Klimov N.I., Mashkov Y.K.

(Rus)

Vol 17, No 3 (2018)

Evaluation of turbine rotor blade life taking into account static and thermal cyclic loading

Badamshin I.K.

(Rus)

Vol 15, No 4 (2016)

Application of structure-energy failure theory for determining the probability of failure and durability of turbine and compressor blades of aircraft engines

Chernyaev A.I., Trefilov V.A.

(Rus)

Vol 15, No 3 (2016)

Suppression of gas-dynamic self-oscillations in the outflow line of a gas control valve

Balyaba M.V., Ermilov M.A., Kryuchkov A.N., Shabanov K.U.

(Rus)

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

Application of stereolithography prototypes for gas dynamic tests

Matveev V.N., Shabliy L.S., Krivcov A.V.

(Rus)

Vol 10, No 5 (2011)

Modeling of propane combustion processes in case of converting a GTE combustion chamber to gaseous fuel

Matveev S.G., Lanskiy A.M., Orlov M.Y., Abrashkin V.Y., Dmitriev D.N., Zubrilin I.A., Semenov A.V.

(Rus)

Vol 14, No 1 (2015)

Computer-aided design of aircraft gas turbine engines and selection of materials for their main parts

Akhmedzyanov D.A., Kishalov A.E., Markina K.V.

(Rus)

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

Design of the gas turbine engine rotor wheel with ceramic blades

Sapronov D.V., Reznik S.V.

(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)

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

Arbekov A.N.

(Rus)

MR vibration dampers development to reduce vibration and noise in gas turbine locomotive and their equivalent vibration tests

Ermakov A.I., Lazutkin G.V., Parovay F.V., Troynikov A.A.

(Rus)

Development liquid roket engine on component fuel liquefied natural gas and oxygen for reusable space launching systems

Efimochkin A.F., Khrisanfov S.P., Golubyatnik V.V., Kafarena P.V., Yeliseyev A.V.

(Rus)

Operational testing of thermoplastic reinforced blades

Krutsilo V.G., Krotinov N.B.

(Rus)

Vol 13, No 1 (2014)

Simulation and research of factors affecting aerodynamic indices of the gas purification process

Usmanova R.R., Zhernakov V.S.

(Rus)

Vol 9, No 2 (2010): Special Issue

Analysis of possibility of residual propellant utilization in Soyuz orbital stage for controllable descent

1 1., 1 1., 1 1., 1 1.

(Rus)

Theoretical calculation approach of gas turbine engines compressor characteristic line

1 1.

(Rus)

Probabilistic estimate of compressor blades durability to foreign object damage

1 1., 1 1.

(Rus)

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

Wearability, wearproof and heat-shielding coverings for details of the gas path of the turbine, the compressor and the chamber of combustion of gas turbine engine

Barvinok V.A., Shitarev I.L., Bogdanovich V.I., Dokukina I.A., Karasev V.M.

(Rus)

Development of an algorithm of design calculation of a combustion chamber for microturbine electric power plants

Matveev S.G., Abrashkin V.Y., Orlov M.Y., Lansky A.M., Makarov N.S., Matveev S.S., Anisimov M.Y.

(Rus)

Vol 19, No 4 (2020)

The effect of heat recovery on the optimal values of helicopter turboshaft engine parameters

Omar H.H., Kuz'michev V.S., Zagrebelnyi A.O., Grigoriev V.A.

(Rus)

Vol 18, No 3 (2019)

Life of gas turbine engine components under corrosive exposure

Pivovarova M.V., Gladkiy I.L.

(Rus)

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

Investigation of resonant oscillations working plates in experimental models of pneumatic valve

Zhuravliov О.A., Komarov S.Y., Makaryants G.M., Sergeev R.N., Harchikova J.V.

(Rus)

Vol 18, No 2 (2019)

Calculation of lubricant flow in the slide bearing of the aviation engine reducer

Siluyanova M.V., Fertikov A.О.

(Rus)

Vol 17, No 4 (2018)

Optimization of fuel distribution in the afterburner of a gas turbine engine

Nelyubin V.R.

(Rus)

Vol 17, No 2 (2018)

Development of a multiuser system web-interface as a tool of using mathematical packages for solving engineering tasks

Danilenko A.N., Zhdanov I.A.

(Rus)

Vol 16, No 3 (2017)

Constructing 3D fan blade models in CAD-system on the basis of coordinate measuring techniques

Arkhipov A.N., Ravikovich Y.A., Fedorov I.M., Kholobtsev D.P.

(Rus)

Vol 15, No 4 (2016)

Mathematical modelling of the working process of a hot gas pressure feed system

Salich V.L.

(Rus)

Vol 10, No 6 (2011)

Estimation of the required thrust impulse for small spacecraft (SSC) control system with a propulsion system using fuel gas components

Titov B.A., Koltsov I.V.

(Rus)

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

Research of hydrodynamic processes in the lubrication system of gas turbine engines

Gulienko A.I., Shchurovskiy Y.M.

(Rus)

Vol 10, No 5 (2011)

Experimental study of swirled gas flow by the particle image velocimetry method

Knysh Y.A., Redkin Y.S., Dmitriev D.N.

(Rus)

Vol 13, No 5-4 (2014): Special Issue

Calculation of exciting aerodynamic load on a gas turbine engine compressor blade induced by the effect of a non-uniform gas flow

Ermakov A.I., Shklovets A.O., Fedorchenko D.G.

(Rus)

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

Validation of CFD-models of gas turbine engine uncooled turbines

Matveev V.N., Popov G.M., Goryachkin E.S., Smirnova Y.D.

(Rus)

On the development of probes for measuring pressure pulsations in the gas-dynamic channel gas generator

Shorin V.P., Gimadiyev A.G., Bystrov N.D., Ilyinsky S.A., Alexandrova T.G.

(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)

The defectoscopy of the fatigue cracks in the gas turbine parts by means of eddy-current method

Porter A.M., Bukatyi S.A., Leshin D.P., Vasilchuk M.V., Galickyi A.A.

(Rus)

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

Use of the dynamic programming method for solving tasks of GTE management optimization using the aircraft efficiency criteria

Tkachenko A.Y., Kuzmichev V.S.

(Rus)

Modelling of an ejector for turbine aeroengines for application in performance synthesis tools

Georgi J., Staudacher S., Falaleev S.V.

(Rus)

Vol 9, No 1 (2010)

Compulsory ignition of fuel-air mixture in small-sized gas turbine engine combustion chambers

1 1., 1 1., 1 1.

(Rus)

Cycle air heating system of gas pumping unit NEVA-25NK

1 1., 1 1., 1 1., 1 1.

(Rus)

the research of the influence of the maximal stress duration in the cycle of loading upon the low-cycle fatigue and the long-term strength of the turbine shaft made of the material ЭИ 961-Ш

1 1., 1 1., 1 1.

(Rus)

Vol 8, No 2 (2009)

Analysis of temperature separation efficiency in vortex gas flows

Biryuk V.V., Kurnosov N.Y., Tarnopolsky A.V.

(Rus)

Mathematical model for calculating radial non-uniformity of the gas temperature field at the exit of small gas turbine engine combustion chambers

Lukachev S.V., Abrashkin V.Y., Lansky A.M., Matveev S.G.

(Rus)

Vol 19, No 4 (2020)

Investigation of the characteristics of the component of vibration of gas turbine engine gearbox that causes fatigue failures of its structural elements in case of tooth flank wear

Sundukov A.E.

(Rus)

Vol 18, No 3 (2019)

Mathematical model for calculating the mass of a heat exchanger in problems of optimizing the parameters of the working process of aircraft gas turbine engines

Kuz'michev V.S., Omar H., Tkachenko A.Y., Bobrik A.A.

(Rus)

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

Influence in a constructive and regime parameters antechamber by operation-in the combustion chamber liquid-propellant rocket engine thrusters on hypergolic liquid propellants

Nigodjuk V.E., Sulinov A.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 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 17, No 2 (2018)

Development and research of a device for gas sheet stamping with a piston pressure multiplier

Botashev A.Y., Bayramukov R.A.

(Rus)

Vol 16, No 2 (2017)

Assessment of gas turbine engine airfoil surface microstructure

Nosov N.V., Abramov A.D., Kosulin S.I.

(Rus)

Vol 15, No 4 (2016)

Method of vibration diagnostics of aerodynamic and aeroelastic oscillations in gas turbine engine compressor

Posadov V.V., Remizov A.E.

(Rus)

Vol 10, No 7 (2011)

Gas mass spectrometer with a non-linear ion mirror

Pijakov I.V., Rodin D.V.

(Rus)

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

Method of investigating the elastohydrodynamic contact in slide bearings with compressible and incompressible lubrication

Temis M.J.

(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 13, No 5-4 (2014): Special Issue

Research of the validity of forecasting low cycle durability of gas turbine engine parts based on Manson’s equation

Porter А.M., Bukatyi S.A., Leshin D.P.

(Rus)

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

Method of gas turbine malfunction diagnostics using hybrid intellectual systems

Antropov P.G., Dolinina O.N., Shvarts A.Y.

(Rus)

Development of techniques and calculation program heterogeneous gas measurement circuits

Gimadiyev A.G., Bystrov N.D., Ustinov A.

(Rus)

Choosing the optimal method of the centrifugal loads modeling using 2D FE models of the compressor’s disks slots

Balyaeva N.N., Guschin A.Y.

(Rus)