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

Dominik Głowacki

Dominik Głowacki

Warsaw University of Technology, Institute of Aeronautics and Applied MechanicsWarsaw,
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Głowacki, Dominik
 e 
Mirosław Rodzewicz

Mirosław Rodzewicz

Warsaw University of Technology, Institute of Aeronautics and Applied MechanicsWarsaw,
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Rodzewicz, Mirosław
  
22 lug 2017
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Pubblicato online: 22 lug 2017
Pagine: 97 - 103
DOI: https://doi.org/10.1515/fas-2016-0008
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© 2016 Dominik Głowacki et al., published by De Gruyter Open
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

[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.Search in Google Scholar

[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.240.191Search in Google Scholar

[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.Search in Google Scholar

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Inglese
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