Effects of Surface Waviness on Fan Blade Boundary Layer Transition and Profile Loss — Part II: Experimental Assessments and Applications

<jats:title>Abstract</jats:title> <jats:p>Part II describes the experimental assessment and the application of the ideas in Part I concerning the mechanisms that determine the role of blade surface waviness on laminar-turbulent transition and their consequent effect...

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Bibliographic Details
Main Authors: Lee, Jinwook, Ramaswamy, Vaishnavi, Spakovszky, Zoltán S, Greitzer, Edward M, Drela, Mark, Talbotec, Jérôme
Other Authors: Massachusetts Institute of Technology. Gas Turbine Laboratory
Format: Article
Language:English
Published: ASME International 2022
Online Access:https://hdl.handle.net/1721.1/145333

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