Abstract
of the shear layer rollup and wake vortex shedding can usually be observed. This study highlights the actuator eects by unsteady actuation with forcing frequencies selected according to the natural frequency of the wake vortex shedding. Mean aerodynamic force measurements, PIV and hot-wire anemometry in the vicinity of the shear layer and in the far wake were performed to characterize the benets of the control. For a deep post-stall airow, results show that forcing frequencies closer to the wake vortex shedding frequency lead to achieve a high increase in lift.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
