Effects of Boundary-Layer Ingestion on the Aero-Acoustics of Transonic Fan Rotors

The use of boundary-layer-ingesting, embedded propulsion systems can result in inlet flow distortions where the interaction of the boundary-layer vorticity and the inlet lip causes horseshoe vortex formation and the ingestion of streamwise vortices into the inlet. A previously-developed body-force-b...

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Bibliographic Details
Main Authors: Defoe, Jeffrey James, Spakovszky, Zoltan S
Other Authors: Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Format: Article
Published: ASME International 2018
Online Access:http://hdl.handle.net/1721.1/114678
https://orcid.org/0000-0003-2167-9860