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

Fan engine research

Murzagaliev A.G., Nekrasov V.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)

Vol 17, No 3 (2018)

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

Ryzhkov V.V., Morozov I.I.

(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)

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

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

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

(Rus)

Vol 21, No 1 (2022)

On the efficiency of using the Navier-Stokes approximation in thermogasdynamic calculation of low-thrust liquid-propellant rocket engines at low Reynolds numbers

Maksimov A.D., Shustov S.A.

(Rus)

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

Issues of evolution of rotor piston engines’ subject abroad and in Russia

Kocherov E.P., Kononov V.A., Okorochkov V.V., Okorochkova V.M., Ivanova K.P.

(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 1 (2015)

Common properties of hydrocarbon combustion products and Brayton cycle

Mikheenkov E.L.

(Rus)

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

Design solutions to provide thermal protection of three-shaft turbofan engine turbine support oil cavities

Petrukhin A.G., Boev A.A., Butylkin S.V.

(Rus)

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

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

Mikheenkov E.L., Nekrasova S.O.

(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)

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

Modernization of serial automobile engines

Aleksencev E.I., Birjuk V.V., Nekljudov A.A., Denisov A.A.

(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 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 10, No 2 (2011)

Design of bimetallic impeller for gas turbine

Magerramova L.A.

(Rus)

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

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 19, No 1 (2020)

Bringing spacecraft into solar-oriented attitude by the measurements of a single-axis angular-rate sensor and an optical solar sensor

Shipov M.G., Steklova A.A., Davydov A.A.

(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

Ways to improve the workflow of liquid rocket thrusters on hypergolic propellants

Nigodjuk V.E., Sulinov A.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)

Vol 19, No 1 (2020)

Mathematical model of the “tank – nozzle” cooling system

Shalay V.V., Shcherban K.V.

(Rus)

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

Heat engine cycle limitations imposed by fuel properties

Mikheyenkov E.L.

(Rus)

Vol 15, No 4 (2016)

Peculiarities of the working process of low-thrust hypergolic-propellant liquid rocket engines with a thrust of less than 1 N

Nigodjuk V.E., Sulinov A.V.

(Rus)

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

Causes of failures of rolling bearings

Zvonarev S.L., Zubko A.I.

(Rus)

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

Oxyhydrogen propulsion device base on water electrolysis and lrest on component H2 + O2 for control system SS

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

(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)

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 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)

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

A technique to estimate efficiency of turbine underplatform friction dampers

Nikhamkin M.S., Sazhenkov N.A.

(Rus)

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

Pulsing chambers of combustion and their application in aerospace engineering

1 1., 1 1., 1 1.

(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 18, No 1 (2019)

Development of the active gas generator for high altitude firing test benches

Salich V.L.

(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)

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

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

Mixing parameters investigations and methods of approach to calculations and development of the thrusters with a spray-centrifugal scheme of NT and NDMH mixing on the confusion chamber wall in considered

1 1.

(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 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 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)

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 3-2 (2009): Special Issue

Probabilistic estimate of compressor blades durability to foreign object damage

1 1., 1 1.

(Rus)

1 - 42 of 42 Items

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