Engineering Journal: Science and InnovationELECTRONIC SCIENCE AND ENGINEERING PUBLICATION
Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
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Methods to compute electrical strength and output electric characteristics of the rectifying diodes and compare their electric parameters

Published: 03.06.2024

Authors: Onufrieva E.V.

Published in issue: #6(150)/2024

DOI: 10.18698/2308-6033-2024-6-2366

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts

Computational study of the various mixture formation schemes and determination of the main factors influencing the working process parameters of the low-thrust rocket engine combustion chamber

Published: 07.12.2023

Authors: Novikov A.V., Andreev E.A., Bardakova E.I.

Published in issue: #12(144)/2023

DOI: 10.18698/2308-6033-2023-12-2325

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts

Results of an experimental study of the electrostatic fields influence on thermal processes in the MS-20 aviation engine oil exposed to its forced convection. Part 2

Published: 07.12.2023

Authors: Altunin V.A., Lvov M.V., Yusupov A.A., Shchigolev A.A., Gortyshov Yu.F., Koreev E.P., Yanovskaya M.L.

Published in issue: #12(144)/2023

DOI: 10.18698/2308-6033-2023-12-2324

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts

Results of an experimental study of the electrostatic fields’ influence on thermal processes in the MS-20 aviation engine oil exposed to its forced convection. Part 1

Published: 27.11.2023

Authors: Altunin V.A., Lvov M.V., Yusupov A.A., Shchigolev A.A., Gortyshov Yu.F., Koreev E.P., Yanovskaya M.L.

Published in issue: #11(143)/2023

DOI: 10.18698/2308-6033-2023-11-2317

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts

A search for recommendations to select numerical model settings for efficient simulation of the working process of the axial turbine blade with convective cooling

Published: 27.11.2023

Authors: Volkov A.A., Popov G.M., Zubanov V.M., Matveev V.N., Baturin O.V.

Published in issue: #11(143)/2023

DOI: 10.18698/2308-6033-2023-11-2316

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts

Analysis of the aircraft gas turbine engine spline coupling with the finite element method and taking into account the loads and the misalignment influence

Published: 27.11.2023

Authors: Nikolaev I.V., Leontiev M.K., Popov V.V., Nizametdinov F.R.

Published in issue: #11(143)/2023

DOI: 10.18698/2308-6033-2023-11-2315

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts