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

Karpov A.V.

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

Research of repeatability of characteristics of multilayered corrugated dampers of aircraft and rocket engines using the Monte-Carlo method

Ponomaryov Y.K.

(Rus)

A technique to estimate efficiency of turbine underplatform friction dampers

Nikhamkin M.S., Sazhenkov N.A.

(Rus)

Vol 9, No 3 (2010)

Questions of economic justification converting aviation engines for use in compressor stations of unified gas supply system

Vorobyov M.Y.

(Rus)

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

Features of the new gas turbine aviation engines theory course

Mingazov B.G., Kosterin V.A., Varsegov V.L.

(Rus)

Vol 20, No 4 (2021)

The structure of knowledge base to support the development of low-thrust liquid-propellant rocket engines based on computer technologies

Ryzhkov V.V.

(Rus)

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 17, No 2 (2018)

Improvement of friction units of power plants by aplying ceramic composite spray coatings

Siluyanova M.V., Fertikov A.O.

(Rus)

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

Experimental studies of prototype models of bimetallic blisks of a high-temperature turbine with cooled blades for advanced gas turbine engines

Magerramova L.A., Stadnikov A.N.

(Rus)

An experimental technique for efficiency assessment of ring dampers for gas turbine engine blisk

Nikhamkin M.S., Balakirev A.A., Voronov L.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)

Applying the possibilities of Microsoft Excel for solving problems of fuel burning thermodynamics

Mikheenkov E.L., Nekrasova S.O., Ramzaeva E.A.

(Rus)

Vol 19, No 1 (2020)

Mathematical model of the “tank – nozzle” cooling system

Shalay V.V., Shcherban K.V.

(Rus)

Bases of methodology of maintenance of system safe operation of engines at all stages of life cycle

Grigoriev V.A., Kuznetsov S.P.

(Rus)

Vol 16, No 2 (2017)

Assessment of a liquid rocket engine concept based on innovative technologies

Solodovnikov A.V., Akinshin I.A., Golubyatnik V.V., Krivonogov A.V.

(Rus)

Vol 14, No 1 (2015)

Common properties of hydrocarbon combustion products and Brayton cycle

Mikheenkov E.L.

(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 3-3 (2009): Special Issue

About the centre of science-educational of laser systems and technologies at faculty DLA SSAU

1 1., 1 1., 1 1.

(Rus)

Limit values of the Brayton cycle with the use of reduced fuel characteristics

Mikheenkov E.L., Nekrasova S.O.

(Rus)

Vol 18, No 4 (2019)

Computer-aided design of low-thust rocket engines using the domain-specific knowledge database and CAE / CAD systems

Ryzhkov V.V., Morozov I.I., Lapshin E.A.

(Rus)

Structure and physico-mechanical properties of heat resistant gazoplazmennyh coating NiCrCoAlY/ZrO2 for turbine blades of gas turbine engines

Tarasenko Y.P., Tsareva I.N., Berdnik O.B., Fehl Y.A.

(Rus)

Vol 16, No 1 (2017)

Evaluation of low cycle fatigue based on the use of Coffin-Manson dependence under zero-to-“soft” loading cycle

Pavlov V.F., Kirpichyov V.A., Kocherova E.E., Zlobin A.S.

(Rus)

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

Development of the technology of diagnostics of turbo-jet aviation engines by a filtering element with a diagnostic layer

Drokov V.V., Drokov V.G., Muryshenko V.V., Mukhutdinov F.I., Khaliullin V.F.

(Rus)

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

Interaction of exhaust jets of rocker propulsions on various propellants with atmosphere for estimation of ecological safety of firing of rockets and launchers

Zavelevich F.S., Ushakov N.N.

(Rus)

Methodology complex of hardware-in-the-loop functional modelling of gas turbines and its systems

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

(Rus)

Correlation and regression model for the assessment of circular non-uniformity of the gas temperature field at the outlet of small gas turbine engine combustion chambers

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

(Rus)

Vol 18, No 3 (2019)

Prospects of application of additive technologies to develop parts and components of gas turbine engines and ramjets

Magerramova L.A., Nozhnitsky Y.A., Volkov S.A., Volkov M.E., Chepurnov V.Z., Belov S.V., Verbanov I.S., Zaikin S.V.

(Rus)

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

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

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

On a method of practical training fulfillment for course of studies “Design of Main Units and Systems of Engine”

Borisov V.A., Zhizhkin A.M.

(Rus)

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

Selection of the design and application of plasma technology protective coatings parts gas turbine engines

Dokukina I.A.

(Rus)

The story of invention and development of supercharge units of internal combustion engines

1 1., 1 1., 1 1.

(Rus)

Method of reduced fuel characteristics and parameters of the operating cycles of heat engines

Anastaseev V.V., Belozertsev S.V., Mikheenkov E.L., Nekrasova S.O.

(Rus)

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

Pressure measurements in the pipelines with the help of combined high temperature pressure sensor

Limanova N.I., Yudin P.E., Limanov I.A.

(Rus)

On the issue of research of the properties of the heat-resistant nickel single-crystal superalloys

Tikhomirova E.A., Zhivushkin A.A., Getsov L.B., Rybnikov A.I.

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

Causes of failures of rolling bearings

Zvonarev S.L., Zubko A.I.

(Rus)

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

Approaches to modeling work of gas turbine engine`s core as a connected task

Krivcov A.V., Shabliy L.S., Baturin O.V.

(Rus)

Pulsing chambers of combustion and their application in aerospace engineering

1 1., 1 1., 1 1.

(Rus)

Vol 17, No 4 (2018)

Propulsion systems and low-thrust rocket engines based on various physical principles for control systems of small and micro-spacecraft

Ryzhkov V.V., Sulinov A.V.

(Rus)

Vol 15, No 4 (2016)

Method of calculating the thickness of the combustion chamber of a liquid rocket engine made with the use of innovative technologies and materials

Krivonogov A.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)

Vol 10, No 2 (2011)

Design of bimetallic impeller for gas turbine

Magerramova L.A.

(Rus)

Decrease in toxicity of transport diesel engines by neutralisation nitrogen oxide of the fulfilled gases

1 q., 1 1.

(Rus)

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

Heat engine cycle limitations imposed by fuel properties

Mikheyenkov E.L.

(Rus)

Vol 17, No 3 (2018)

Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines

Ryzhkov V.V., Morozov I.I.

(Rus)

Vol 15, No 4 (2016)

Efficiency of aft diffusers in vacuum systems of test benches for high-altitude firing tests of low-thrust liquid rocket engines

Galperin R.N., Gulyaev Y.I., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.

(Rus)