Ice accretion prediction on an engine inlet

Date

2015-09-10

Author

Özgen, Serkan
Görgülü, İlhan
Tatar, Volkan

Metadata

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URI

https://hdl.handle.net/11511/83861
http://www.ae.metu.edu.tr/~ae716/lecture-12.pdf

Conference Name

8th Ankara International Aerospace Conference (2015)

Collections

Department of Aerospace Engineering, Conference / Seminar

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ICE ACCRETION PREDICTION ON HORIZONTAL AXIS WIND TURBINE BLADES Yırtıcı, Özcan; Özgen, Serkan; Tuncer, İsmail Hakkı (2015-09-10)
Ice accretion simulation on multi-element airfoils using extended Messinger model Özgen, Serkan (Springer Science and Business Media LLC, 2009-01-01) In the current article, the problem of in-flight ice accumulation on multi-element airfoils is studied numerically. The analysis starts with flow field computation using the Hess-Smith panel method. The second step is the calculation of droplet trajectories and droplet collection efficiencies. In the next step, convective heat transfer coefficient distributions around the airfoil elements are calculated using the Integral Boundary-Layer Method. The formulation accounts for the surface roughness due to ice a...
Ice Accretion Prediction on Wind Turbine Blades Under Atmospheric Icing Conditions Yırtıcı, Özcan; Özgen, Serkan; Tuncer, İsmail Hakkı (null; 2016-01-23)
Ice Accretion Prediction on Engine Nacelles in Liquid Phase Clouds Özgen, Serkan; Görgülü, İlhan; Tatar, Volkan (null; 2015-09-22) More than a hundred in-flight incidences have been reported in the last two decades related to icing on aircraft engine components including rollbacks, mechanical failure and flameouts [1, 2]. Thus, in-flight ice accretion on aircraft engine components and nacelles has been attracting more interest, especially from the airworthiness certification point of view. Computer simulations as well as ground and flight tests are among the means of compliance for airworthiness certification related to safe flight in ...

Citation Formats

S. Özgen, İ. Görgülü, and V. Tatar, “Ice accretion prediction on an engine inlet,” presented at the 8th Ankara International Aerospace Conference (2015), Ankara, Türkiye, 2015, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/83861.