The Effects of a Leading Edge Rotating Cylinder on the Performance of a NACA 0015 Airfoil at High Angles of Attack (AIAA 2014-0540)
Conference, AIAA atmospheric flight mechanics ; 2014 ; National Harbor, MD
2014-01-01
14 pages
Includes bibliographical references and author index
Aufsatz (Konferenz)
Englisch
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