Correction: CFD study on NACA 4415 airfoil implementing spherical and sinusoidal Tubercle Leading Edge

[This corrects the article DOI: 10.1371/journal.pone.0183456.].

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Bibliographic Details
Published in:PloS one 2017-11, Vol.12 (11), p.e0188792-e0188792
Main Authors: Aftab, S M A, Ahmad, K A
Format: Article
Language:English
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Summary:[This corrects the article DOI: 10.1371/journal.pone.0183456.].
ISSN:1932-6203
1932-6203
DOI:10.1371/journal.pone.0188792