Detached Eddy Simulation of Flow over NACA0012 Airfoil at High Angle of Attack with Spectral Difference Method (AIAA 2014-0425)
52nd, Aerospace sciences meeting; held at the AIAA SciTech Forum 2014 ; 2014 ; National Harbor, MD
01.01.2014
15 pages
Includes bibliographical references and author index
Aufsatz (Konferenz)
Englisch
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