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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 |
