The Elaboration of the Method of Fatigue Testing of the Rotor of the Mosups Plane Propulsion System

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Open Access

|Jul 2017

References

[1] Bogdanski K., Krusz W., Rodzewicz M. Rutkowski M. “Design and optimization of low speed ducted fan for a new generation of joined wing aircraft” ICAS 2014.
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[2] Bogdański Krzysztof, Głowacki Dominik, Rodzewicz Mirosław: Research on the rotor of a ducted fan propulsion system of MOSUPS aircraft taking into account self balance during operation, w: Solid State Phenomena, Trans Tech Publications, vol. 240, 2016, pp. 191-197.10.4028/www.scientific.net/SSP.240.191
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[3] Głowacki Dominik, Rodzewicz Mirosław: Badania dynamiczne wirnika napędu otunelowanego samolotu MOSUPS, w: Mechanika w Lotnictwie T I / Sibilski Krzysztof (red.), 2014, Polskie Towarzystwo Mechaniki Teoretycznej i Stosowanej, ISBN 978-83-932107-3-2, ss. 49-63.
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DOI: https://doi.org/10.1515/fas-2016-0008 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738

Language: English

Page range: 97 - 103

Published on: Jul 22, 2017

In partnership with: Paradigm Publishing Services

Publication frequency: 1 issue per year

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© 2017 Dominik Głowacki, Mirosław Rodzewicz, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.