Numerical Study of Transient Behavior of a NACA 0008 Airfoil Equipped with a Gurney Flap Using a Control-Volume Based Finite-Element Collocated Scheme (AIAA 2014-1109)
52nd, Aerospace sciences meeting; held at the AIAA SciTech Forum 2014 ; 2014 ; National Harbor, MD
2014-01-01
11 pages
Includes bibliographical references and author index
Conference paper
English
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