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An integrated approach to creating a geometric model of a turbojet engine combustion chamber via reverse engineering
| Authors: Matveev Yu.V., Balakin A.M., Kanakin M.K., Laptev M.A., Barskov V.V., Nurkov I.R. | Published: 05.10.2026 |
| Published in issue: #10(799)/2026 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: reverse engineering, 3D scanning, combustion chamber, turbojet engine, CAD |
Methods in forcing a gas turbine engine
| Authors: Pismennyi V.L. | Published: 17.09.2024 |
| Published in issue: #9(774)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: gas turbine engine, stoichiometric engine, hypersonic aviation, hyperboost, turbine boost, turbojet engine, methods of boosting a gas turbine engine |
Hyper Afterburner Jet Engines
| Authors: Pismennyi V.L. | Published: 13.01.2020 |
| Published in issue: #1(718)/2020 | |
| Category: Aviation, Rocket and Technology | Chapter: Aerodynamics and Heat Transfer Processes in Aircraft | |
| Keywords: hyper force, gas turbine engines, ramjet engine, turbojet engine, hypersonic flight speed |
Computational study of characteristics of intake flow in model axial compressor with regard to different variants of “active disk” boundary condition
| Authors: Voronich I.V., Nguyen V.H. | Published: 20.05.2019 |
| Published in issue: #5(710)/2019 | |
| Category: Aviation, Rocket and Technology | Chapter: Aerodynamics and Heat Transfer Processes in Aircraft | |
| Keywords: turbojet engine, axial compressor air intake, active disk, variables profiles, computational technique |