Analysis of Fan Stage Design Attributes for Boundary Layer Ingestion

Analysis of Fan Stage Design Attributes for Boundary Layer Ingestion

This paper describes a new conceptual framework for threedimensional turbomachinery flow analysis and its use to assess fan stage attributes for mitigating adverse effects of inlet distortion due to boundary layer ingestion (BLI). A non-axisymmetric throughflow method has been developed to describe...

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Bibliographic Details
Main Authors: Hall, David Kenneth, Greitzer, Edward M, Tan, Choon S
Other Authors: Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Format: Article
Published: ASME International 2018
Online Access:http://hdl.handle.net/1721.1/115333
https://orcid.org/0000-0002-2343-910X
https://orcid.org/0000-0001-9625-1020
https://orcid.org/0000-0002-8805-5289

Internet

http://hdl.handle.net/1721.1/115333
https://orcid.org/0000-0002-2343-910X
https://orcid.org/0000-0001-9625-1020
https://orcid.org/0000-0002-8805-5289

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