Features of a Laminar Separated Boundary Layer Near the Leading-Edge of a Model Airfoil for Different Angles of Attack: An Experimental Study

Title
Features of a Laminar Separated Boundary Layer Near the Leading-Edge of a Model Airfoil for Different Angles of Attack: An Experimental Study
Authors
Keywords
-
Journal
Publisher
ASME International
Online
2016-09-06
DOI
10.1115/1.4034606

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