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...

Full description

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

Internet

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

Similar Items