Page 24. Heat engines (except steam engines) UDC: 621.4

Multi-objective optimization workflow uncooled three-stage axial low pressure turbine

Popov Grigory, Goryachkin Evgeny, Novikova Julia, Zubanov Vasily, Volkov Andrei, Korneeva Anastasia

Comparison of algorithms of construction of associative rules on the basis of the data set of customer transactions

Olyanich Igor

Theoretical-probabilistic estimation of the volume of work in progress in the assembly of the turbine wheel

Bolotov Michael, Efremova Tatyana, Yanyukina Mariya

Development of methods for improving the accuracy of the milling of the GTE compressor blade airfoil

Guzev Dmitry, Sokolov Grigory, Zhidyaev Alexey

Improvement of the calibration process of heat flux sensors for space devices' thermal-volume tests

Zagidullin Radmir, Mitroshkina Tatyana, Visotskaya Maria

Drilling rock bit for horizontal wells small diameter

Bogomolov Rodion

Method for estimating the energy and mass-dimension characteristics of an auxiliary propulsion system with fuel cells

Gordin Mikhail, Rogalev Nikolai, Averkov Igor, Baikov Aleksey, Shevchenko Igor

Forecast of extreme air pollution by water and road transport

Lozhkin V.N.

Prospects for the use of gas-motor fuel in Russia

Aleksankov A.M.

History of the arterial tonometer and the “Pranayama” gadget

Igor S. Yavelov, Georgy L. Danielyan, Leonid P. Potak, Andrey V. Rochagov, Anatoly V. Zholobov, Oleg I. Yavelov, Eugeny V. Kolosov

Method for estimation of the pulse wave propagation velocity by a manual pneumatic arterial pressure sensor

Antsiperov V.E., Bugaev A.S., Danilychev M.V., Mansurov G.K.

The method of the disk friction determining of low mass flow centrifugal pumps

Zuev A. A., Nazarov V. P., Arngold A. A., Petrov I. M.

Modeling of the stress-strain state of rocket-space technology structural elements manufactured by using additive technologies

Ushakova E. S.

Features and modernization methods of thrust measurement devices for liquid rocket engine test stands

Begishev A. M., Zhuravlev V. Y., Torgashin А. S.

Design of a multifunctional electric propulsion subsystem of the spacecraft

Yu. M. Ermoshkin, Yu. V. Kochev, D. V. Volkov, E. N. Yakimov, A. A. Ostapushchenko

The influence of the method of fuel supply into the combustion chamber on the quality of mixing and on the carbon oxide formation

A. V. Baklanov

Heat transfer in the centrifugal force field for gas turbines elements

A. A. Zuev, A. A. Arngold, E. V. Khodenkova

CFD methods for cavitation modeling in centrifugal and axial pumps of LRE

A. S. Torgashin, D. A. Zhujkov, V. P. Nazarov, A. M. Begishev, A. V. Vlasenko

The possibility of using methane-hydrogen fuel in converted gas turbine engines for power plants

Baklanov A. V.

Influence of filling processes for mixing head of gas generators on dynamics of liquid rocket engine without starter device

Belayev E.N., Vorobyev A.G.

The method of the disk friction determining of low mass flow centrifugal pumps

Zuev A.A., Nazarov V.P., Arngold A.A., Petrov I.M.

Modeling of the stress-strain state of rocket-space technology structural elements manufactured by using additive technologies

Ushakova E.S.

Features and modernization methods of thrust measurement devices for liquid rocket engine test stands

Begishev A. M., Zhuravlev V. Y., Torgashin A. S.

Design of a multifunctional electric propulsion subsystem of the spacecraft

Ermoshkin Yu. M., Kochev Yu. V., Volkov D.V., Yakimov E.N., Ostapushchenko A.A.

The influence of the method of fuel supply into the combustion chamber on the quality of mixing and on the carbon oxide formation

Baklanov A.V.

Heat transfer in the centrifugal force field for gas turbines elements

Zuev A.A., Arngold A.A., Khodenkova E.V.

CFD methods for cavitation modeling in centrifugal and axial pumps of LRE

Torgashin A.S., Zhujkov D.A., Nazarov V.P., Begishev A.M., Vlasenko A.V.

The possibility of using methane-hydrogen fuel in converted gas turbine engines for power plants

Baklanov A.V.

Аpplication of the propulsion subsystem on the base of SPT-100V plasmic thruster to orbit raising and orbit control of the Express-80 and Express-103 spacecraft

Ermoshkin Yu. M., Vnukov A.A., Volkov D.V., Kochev Yu. V., Simanov R.S., Yakimov E.N., Grikhin G.S.

Comparative analysis of verified numerical simulation of cavitation based on the Rayleigh - Plesset model for liquid propellant rocket engine pumps

Torgashin A. S., Zhujkov D. A., Nazarov V. P., Begishev A. M., Vlasenko A. V.

Alternative to the theory of inversible processes

Valery A. Etkin

Analysis of the stress-deformed state of the prismatic support of the lever-grading device of test stands for liquid rocket engines

Begishev A.M., Zhuravlev V.Y., Nazarov V.P., Torgashin A.S.

Dynamics of the flow in the sections of the elements of the supply path of the turbopump unit of the LRE

Arngold A.A., Zuev A.A., Tolstopyatov M.I., Dubynin P.A.

Design technology of complex dies on the basis theory of adaptability

Nosov N.V.

Method of calculating surface roughness during abrasive treatment

Grishin R.G., Nosov N.V., Salnikov I.M., Gordienko Ya.M., Ladyagin R.V.

Local heat transfer parameters in the areas of the developing temperature boundary layer in the cavities of gas turbines

Zuev A.A., Arngold A.A., Falkova E.V., Tolstopyatov M.I., Dubynin P.A.

Method for processing the results of cavitation tests of TNA pumps in order to obtain an approximating function

Torgashin A.S., Zhujkov D.A., Nazarov V.P., Begishev A.M.

The feature of the “Express-AMU3”, “Express-AMU7” spacecrafts injecton to geostationary orbit

Ermoshkin Yu. M., Vnukov A.A., Volkov D.V., Kochev Yu. V., Simanov R.S., Yakimov E.N., Pridannikov S. Yu.

Methodology for assessing reliability of stand-bed systems in testing liquid throat engines

Nazarov V.P., Piunov V. Yu., Kolomentsev A.I., Yatsunenko V.G., Golikovskaya K.F.

Create a digital twin of the compressor impeller assembly process

Pechenina E.Yu.

Heat engines (except steam engines) - 621.4

Scientific articles