Kinematic Design and Control Analysis of A Subsonic Ejector Nozzle with Omni-Directional Thrust Vectoring for Afterburning Turbofan Engines
By: Igor Oganyan and Vasyl Loginov
DOI: https://doi.org/10.2478/tar-2025-0018 | Journal eISSN: 2545-2835
Language: English
Page range: 45 - 68
Submitted on: Aug 18, 2025
|Accepted on: Oct 23, 2025
|Published on: Dec 24, 2025
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year
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© 2025 Igor Oganyan, Vasyl Loginov, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.