Effects of Burst Frequency and Momentum Coefficient of DBD Actuator on Control of Deep-stall Flow around NACA0015 at Re~c=2.6x10^5 (AIAA 2014-0766)
52nd, Aerospace sciences meeting; held at the AIAA SciTech Forum 2014 ; 2014 ; National Harbor, MD
2014-01-01
16 pages
Includes bibliographical references and author index
Aufsatz (Konferenz)
Englisch
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