Effect of the Reynolds Number on the Performance of a NACA0012 Wing with Leading Edge Protuberance at Low Reynolds Numbers

Published 2018 View Full Article

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Title
Effect of the Reynolds Number on the Performance of a NACA0012 Wing with Leading Edge Protuberance at Low Reynolds Numbers
Authors
Keywords
Passive separation control, Leading edge protuberance, NACA0012 airfoil, Low Reynolds number
Journal
FLOW TURBULENCE AND COMBUSTION
Volume -, Issue -, Pages -
Publisher
Springer Nature America, Inc
Online
2018-09-01
DOI
10.1007/s10494-018-9978-3
References
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