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

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

Bibliographic Details
Main Authors:	S M A Aftab, K A Ahmad
Format:	Article
Language:	English
Published:	Public Library of Science (PLoS) 2017-01-01
Series:	PLoS ONE
Online Access:	http://europepmc.org/articles/PMC5697840?pdf=render

Internet