Computational fluid dynamics simulations of ship airwake with a hovering helicopter rotor

Date

2016-01-01

Author

Orbay, Ezgi
Sezer Uzol, Nilay

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Computational Fluid Dynamic simulations of ship airwake are performed together with an actuator disk model for a rotor model hovering over the flight deck. The flow around Simple Frigate Shape 2 (SFS2) is computed in steady-state and unsteady conditions by solving RANS and hybrid RANS/LES equations. The unstructured grid is generated for the ship geometry. Also, an actuator disk is added into the model to investigate downwash effect of rotor on ship airwake and interaction of rotor and ship airwake.

Subject Keywords

Actuator Disk Model, Computational Fluid Dynamics (CFD), Helicopter Rotor, Ship Airwake

URI

https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85086288047&origin=inward
https://hdl.handle.net/11511/96929

Conference Name

9th International Conference on Computational Fluid Dynamics, ICCFD 2016

Collections

Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

E. Orbay and N. Sezer Uzol, “Computational fluid dynamics simulations of ship airwake with a hovering helicopter rotor,” presented at the 9th International Conference on Computational Fluid Dynamics, ICCFD 2016, İstanbul, Türkiye, 2016, Accessed: 00, 2022. [Online]. Available: https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85086288047&origin=inward.