Active Flow Control and Global Stability Analysis of Separated Flow over a NACA 0012 Airfoil
The objective of this computational study is to examine and quantify the influence of fundamental flow control inputs in suppressing flow separation over a canonical airfoil. Most flow control studies to this date have relied on the development of actuator technology, and described the control input...
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| Format: | Others |
| Language: | English English |
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Florida State University
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| Online Access: | http://purl.flvc.org/fsu/fd/FSU_2017SP_Munday_fsu_0071E_13086 |