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...
Main Authors: | Lee, Jinwook, Spakovszky, Zoltán S, Greitzer, Edward M, Drela, Mark, TALBOTEC, Jérôme |
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Other Authors: | Massachusetts Institute of Technology. Gas Turbine Laboratory |
Format: | Article |
Language: | English |
Published: |
ASME International
2022
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Online Access: | https://hdl.handle.net/1721.1/145335 |
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