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Operational testing of thermoplastic reinforced blades

Krutsilo V.G., Krotinov N.B.

(Rus)

Guaranteeing of ecological and economic indicators of internal combustion engine

Grabovskiy A.A., Mironov V.A.

(Rus)

Vol 10, No 1 (2011)

Optimal program of controlling continuous low thrust in the flight between noncoplanar elliptical and geostationary orbits

Fadeenkov P.V., Ishkov S.A.

(Rus)

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

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

1 1., 1 1., 1 1.

(Rus)

Development and study of the designs of sprayers with increased speed for internal combustion engine (ice)

, ,

(Rus)

Increasing efficiency of pressurization of the rocket tanks in the flight

1 1., 1 1.

(Rus)

Seal designing in a structure of the cooling system in gas turbine engine

Vinogradov A.S., Myatlev A.S.

(Rus)

Vol 12, No 1 (2013)

Optimal control of the angle of attack of a hypersonic flight vehicle

Bebyakov A.A.

(Rus)

Vol 12, No 4 (2013)

The usage of high power supply capacity transport spacecraft

Ivanovich S.N.

(Rus)

Vol 19, No 4 (2020)

Development of improved performance electromagnetic valve for liquid rocket engine

Igolkin A.A., Chubenko T.A., Maksimov A.D.

(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 3-4 (2011): Special Issue

Test bench for investigation of thrusters intra-chamber working processes

Pervyshin A.N., Ryazanov A.I.

(Rus)

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

Physical workflow model in the combustion chamber LREST with a jet-centrifugal jets on hypergolic propellants

Silyutin M.V., Shustov S.A.

(Rus)

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

Calculation of indicator diagram dynamic test at internalcombustion engine in KDAM environment

Kosenok B.B.

(Rus)

Vol 18, No 2 (2019)

Technology of computational analysis of the working process parameters of low-thrust rocket engines running on gaseous oxygen-hydrogen fuel with the use of ANSYS CFD

Ryzhkov V.V., Morozov I.I.

(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 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 3 (2017)

Locally optimal control of space tug motion between the libration points of the Earth-Moon system

Starinova O.L., Fain M.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)

The influence of booster design features on aicraft engine fan tonal noise

Khaletskiy Y.D., Korzhnev V.N., Pochkin Y.S.

(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 14, No 2 (2015)

Strength analysis of internal combustion engine elements by using ANSYS with taking into account heat processes in the combustion chamber

Biryuk V.V., Gorshkalev A.A., Kayukov S.S., Saigakov E.A.

(Rus)

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

Modeling of intrachamber processes in an oxygen-hydrogen thruster

Vaulin S.D., Salich V.L.

(Rus)

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

Verification of energy efficiency of a low-thrust liquid-propellant engine with the deflector-centrifugal injecting pattern

Ageenko Y.I., Pegin I.V.

(Rus)

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

The influence of the shuttle effect on the intensification of heat losses in a Stirling engine

Savchenko V.A., Stolyarov S.P.

(Rus)

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

Seal designing as element of aircraft engine systems and engine units

Vinogradov A.S.

(Rus)

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

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)

Vol 11, No 2 (2012)

Joint works of Ilyushin design bureau and general designer N. D. Kuznetsov

Novozhilov G.V.

(Rus)

The projecting of gas turbine engine composite blades

Ryzhov A.A., Galimkhanov B.K., Ryzhov N.A., Latypov R.K., Irgalin S.R.

(Rus)

Vol 13, No 1 (2014)

Development of a small-sized acoustic probe for the measurement of pressure pulsations in the gasdynamic duct of gas turbine engines

Gimadiyev A.G., Bystrov N.D., Ilyinsky S.A.

(Rus)

Vol 9, No 4 (2010)

Parametric analysis of thermoacoustic travelling-wave engine operation with external heat application

Dovgyallo A.I., Zynovyev Y.A., Vorotnikov G.V.

(Rus)

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

Experimental determination of the side forces acting on the combustion chamber in the altitude chamber at startup

, , , ,

(Rus)

Application’s ways of gas–turbine power plants of NK-family for upgrading of heat electric generation plant

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

(Rus)

Operate reliability enhancement of thermogenerator modules for heat engine with acoustic emission method

1 1.

(Rus)

Project of 30 000 h.p. power gas turbine

Zrelov V.A.

(Rus)

Vol 12, No 2 (2013)

Flame propagation velocity and ionization in burning gasoline and methane with addition of hydrogen

Shaykin A.P., Ivashin P.V., Galiev I.R.

(Rus)

Vol 20, No 3 (2021)

Introduction to the problem of calculating the parameters of the mixing chamber of an afterburning bypass engine

Karev O.D.

(Rus)

Vol 19, No 3 (2020)

Improving the efficiency of aviation turbofan engines by using an intercooler and a recuperative heat exchanger

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

(Rus)

Vol 18, No 3 (2019)

Gas dynamic calculation of detonation in constant-cross-section ducts

Grigoriev A.V., Rudakov O.A., Solovieva A.V.

(Rus)

Vol 10, No 3-4 (2011): Special Issue

Aspects of the numerical method calculating thermogazodynamic lrest based on not perfect passing of workflows in the combustion chamber

Silyutin M.V., Shustov S.A.

(Rus)

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

Method of design calculation jet-centrifugal gas-liquid duplex fuel nozzle with internal mixing

Egorychev V.S.

(Rus)

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

Testing of combined air-rocket engine mak-up with pulsing combustion chamber

Solodovnikov A.V., Vishegorodcev E.N., Golubyatnik V.V.

(Rus)

Vol 18, No 1 (2019)

Development of blend composition of aviation kerosene surrogate for the simulation of workflow of gas turbine engine combustion chamber

Matveev S.G.

(Rus)

Vol 17, No 4 (2018)

Proposals for improving the efficiency and service life of the turbines of turbo-pump assemblies in liquid-propellant rocket engines by using double-sided crest-type radial labyrinth seals

Levochkin P.S., Chvanov V.K., Vasiliev V.S., Timushev S.F.

(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 16, No 3 (2017)

Selecting a squeeze film damper model for solving problems of gas turbine engine rotor dynamics

Leontiev M.K., Kutakov M.N.

(Rus)

Vol 15, No 4 (2016)

Unstady heat-mass-transfer and fuel distributions in flows downstream the gas-dynamic flame holder

Tretyakov V.V., Sviridenkov A.A.

(Rus)

Vol 15, No 2 (2016)

Empirical metod of predicting aviation piston engine noise

Moshkov P.A.

(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 14, No 1 (2015)

Possibility of using a bi-directional impulse turbine in a thermo-acoustic engine

Dovgjallo A.I., Shimanov A.A.

(Rus)

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

Development of thruster chamber operating on oxygen-hydrogen fuel

Salich V.L.

(Rus)

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

Results of experimental studies of parameters of low-thrust rocket engines operating on gaseous oxygen-hydrogen fuel

Ageenko Y.I., Lapshin E.A., Morozov I.I., Pegin I.V., Ryzhkov V.V.

(Rus)

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

CFD-modeling of processes in a high-pressure oxidizer pump for the turbopump assembly of a liquid rocket engine

Zubanov V.M., Shabliy L.S.

(Rus)

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

Oxygen-hidrogen liquid rocket engine using turbo-pump developed for aviation hidrogen liquid two-spool turbo-jet

Ivanov A.I., Borisov V.A.

(Rus)

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

Robust research of the fuzzy logic controllers using a fuel flow control loop of the gas-turbine engine as an example

Chicherova E.V.

(Rus)

Vol 11, No 2 (2012)

Numerical simulation of gas temperature spatial distribution in a full-size gas turbine combustor and its one-burner sector

Kostyuk V.Y., Kirilash Y.I., Stasyuk A.V., Shein V.V., Karzov D.V.

(Rus)

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

Increasing the overall performance of a two-stroke engine with spark ignition by fuel injection

Dovgyallo A.I., Krasheninnikov S.V., Shchepetov D.A.

(Rus)

Problems and prospect of microgasturbines development for unmanned aerial vehicle propulsion

Zhdanov I.A., Staudacher S., Falaleev S.V.

(Rus)

Vol 10, No 2 (2011)

Construction of a blade beam finite element as a component of the blade disk rotary-symmetrical system

Davydov D.P.

(Rus)

Vol 9, No 4 (2010)

Development of turbopump unit design for hydrogen liquid-propellant rocket engines without generators developed at the design bureau of chemical automation

Dmitrenko A.I., Ivanov A.V., Rachuk V.S.

(Rus)

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

Experimental development of the LRE with CCCM nozzle’s extension

(Rus)

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)