Icing Simulations on Engine Intake

Date

2017-07-03

Author

Uğur, Nermin
Özgen, Serkan
Görgülü, İlhan
Tatar, Volkan

Metadata

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In the present study, the aim is to predict ice accumulation on a 2-D commercial engine intake. The developed tool mainly consists of four modules: modules for the calculation of the flow-field, droplet trajectories and collection efficiencies, thermodynamics and ice accretion. The flow-field solution is done by a panel method modified for the intake geometry and the required engine mass flow rate using a superposition technique. The droplet trajectories are computed using the Lagrangian approach, while the Extended Messinger Model is implemented in the ice accretion module. The results are compared with numerical literature data.

URI

https://hdl.handle.net/11511/73577
https://www.eucass.eu/doi/EUCASS2017-269.pdf

DOI

https://doi.org/10.13009/EUCASS2017-269

Conference Name

7th European Conference for Aeronautics and Space Sciences

Collections

Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

N. Uğur, S. Özgen, İ. Görgülü, and V. Tatar, “Icing Simulations on Engine Intake,” presented at the 7th European Conference for Aeronautics and Space Sciences, Milan, İtalya, 2017, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/73577.