Influence Factors for Impact Actions and Transient Trajectories of Fan Blades after Fan Blade Out in Typical 2-Shaft High Bypass Ratio Turbofan Engine-Reference-Cited by-同舟云学术

Influence Factors for Impact Actions and Transient Trajectories of Fan Blades after Fan Blade Out in Typical 2-Shaft High Bypass Ratio Turbofan Engine

Published:2022-01 Issue:1 Volume:31 Page:96-110
ISSN:1003-2169
Container-title:Journal of Thermal Science
language:en
Short-container-title:J. Therm. Sci.

Author:

Xu Xue,Li Hongxin,Feng Guoquan

Publisher

Springer Science and Business Media LLC

Subject

Condensed Matter Physics

Link

https://link.springer.com/content/pdf/10.1007/s11630-022-1556-2.pdf

Reference19 articles.

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2. CCAR-33R2 Airworthiness standards: Aircraft engines. Civil Aviation Administration of China, Beijing, China, 2011.

3. Federal aviation administration: turbine engine rotor blade containment/durability: advisory circular 33-5. United States Department of Transportation, Washington D.C., U.S., 1990.

4. CS-25 certification specifications for large aeroplanes. European Aviation Safety Agency, Cologne, Germany, 2013.

5. Sinha S., Dynamic characteristics of a flexible bladed-rotor with coulomb damping due to tip-rub. Journal of Sound and Vibration, 2004, 273: 875–919.

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