Analysis of Fan Stage Conceptual Design Attributes for Boundary Layer Ingestion

Analysis of Fan Stage Conceptual Design Attributes for Boundary Layer Ingestion

This paper describes a new conceptual framework for three-dimensional 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 nonaxisymmetric throughflow analysis has been developed to define...

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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/1721.1/114790 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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