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Mathematical modeling of the change in injection pressure during the transition to mixed fuel, taking into account dynamic effects, wave processes and fuel compressibility
| Authors: Buzikov Sh.V., Motovilova M.V. | Published: 25.09.2026 |
| Published in issue: #10(799)/2026 | |
| Category: Energy and Electrical Engineering | Chapter: Turbomachines and Piston Engines | |
| Keywords: nozzle, mixed fuel, flow coefficient, injection pressure, mathematical modelin |
Development and validation of a CFD model of a ducted fan for a low speed aircraft
| Authors: Marakueva O.V., Fedechkin K.S., Salatov V.N. | Published: 27.08.2026 |
| Published in issue: #9(798)/2026 | |
| Category: Energy and Electrical Engineering | Chapter: Turbomachines and Piston Engines | |
| Keywords: ducted fan, tiltrotor, validation, computational fluid dynamics, CFD model, wind tunnel |
Analysis of the influence of extraction chamber non-uniformity flow in a steam turbine on the post-extraction stage
| Authors: Trokhin D.A., Mitrokhova O.M., Muraveyko A.S. | Published: 21.08.2026 |
| Published in issue: #9(798)/2026 | |
| Category: Energy and Electrical Engineering | Chapter: Turbomachines and Piston Engines | |
| Keywords: steam turbine, regenerative steam extraction, extraction chamber, circumferential non-uniformity, post-extraction stage, numerical simulation |
Design and operational features of rocket engines turbopumps turbine-pump intershaft seal systems. Part I. Separation of the same reaction components
| Authors: Ivanov A.V. | Published: 19.08.2026 |
| Published in issue: #8(797)/2026 | |
| Category: Energy and Electrical Engineering | Chapter: Turbomachines and Piston Engines | |
| Keywords: turbine-pump intershaft seal, turbopump assemblies, turbine-pump intershaft seal system, pressure drop |
A model of flow through an area discontinuity with a discharge coefficient: computation algorithm and validation for unsteady gas flow
| Authors: Enikeev R.D., Chernousov A.A. | Published: 13.08.2026 |
| Published in issue: #8(797)/2026 | |
| Category: Energy and Electrical Engineering | Chapter: Turbomachines and Piston Engines | |
| Keywords: unsteady flow, 1D model, local resistance, discharge coefficient, compound pipeline, finite-amplitude waves |
Ensuring modularity of the design of the system of supporting brackets for the intake and exhaust systems of a diesel internal combustion engine for locomotive (or marine) purposes
| Authors: Zakharov М.О., Kozrinov D.А., Grigoryev N.I., Padalyak D.L., Krotov V.М. | Published: 13.08.2026 |
| Published in issue: #8(797)/2026 | |
| Category: Energy and Electrical Engineering | Chapter: Turbomachines and Piston Engines | |
| Keywords: internal combustion engine, intake and exhaust systems, system of supporting brackets, modularity of design |
Experimental study of the two-stroke engine equipped with a side outlet in the exhaust system pipeline
| Authors: Garipov M.D., Enikeev R.D., Zinnatullin R.F., Melkov A.A., Sakulin R.Y., Khalilov E.M. | Published: 13.07.2026 |
| Published in issue: #7(796)/2026 | |
| Category: Energy and Electrical Engineering | Chapter: Turbomachines and Piston Engines | |
| Keywords: two-stroke aircraft engine, tuned exhaust system, compression wave, expansion wave, outlet in pipeline, expansion chamber |
Development of a method for calculating medium-power steam turbines for nuclear power plants using CFD code in the NUMECA software package
| Authors: Trokhin D.A., Zaryankin V.A., Volzentsov A.A. | Published: 26.06.2026 |
| Published in issue: #7(796)/2026 | |
| Category: Energy and Electrical Engineering | Chapter: Turbomachines and Piston Engines | |
| Keywords: steam turbine, flow path, steam humidity, CFD code, NUMECA software, NPP |
Burnout mechanism of a piston made of high-silicon aluminum alloy for internal combustion engines
| Authors: Doynikov A.I., Dudareva N.Yu. | Published: 07.05.2026 |
| Published in issue: #5(794)/2026 | |
| Category: Energy and Electrical Engineering | Chapter: Turbomachines and Piston Engines | |
| Keywords: internal combustion engine, burnout, high-silicon aluminum alloy |
On the issue of increasing the efficiency of the workflow in the combustion chamber of the evaporative type of aviation gas turbine engines when operating on fuel with an anti-turbulent additive
| Authors: Yanovskiy L.S., Arefyev K.Yu., Popov I.M., Abramov M.A., Borovik I.N., Ezhov V.M. | Published: 14.04.2026 |
| Published in issue: #4(793)/2026 | |
| Category: Energy and Electrical Engineering | Chapter: Turbomachines and Piston Engines | |
| Keywords: aircraft engine, kerosene TC-1, polyisobutylene, ignition induction period, combustion coefficient, combustion chamber of an aircraft engine |