Effects of Surface Waviness on Fan Blade Boundary Layer Transition and Profile Loss — Part I: Methodology and Computational Results

<jats:title>Abstract</jats:title> <jats:p>This two-part paper describes a new approach to determine the effect of surface waviness, arising from manufacture of composite fan blades, on transition onset location movement and hence fan profile losses. The approach inc...

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Bibliographic Details
Main Authors: Lee, Jinwook, 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/1721.1/145332