TY - GEN
T1 - Control of a semi-circular planform wing in a "gusting" unsteady free stream flow II
T2 - Modeling and feedback design
AU - Tadmor, Gilead
AU - Williams, David R.
AU - Collins, Jesse
AU - Colonius, Tim
AU - Rowley, Clarence Worth
PY - 2008
Y1 - 2008
N2 - Active flow control has been demonstrated in Part I of this article to modify the lift, drag and pitching moments on a semi-circular wing during "gusting" flow conditions. The low aspect ratio wing, AR = 2.54, is mounted on a captive trajectory system that responds to the instantaneous lift force and pitching moment and the "gusting" flow is simulated by a 0.2 Hz oscillation of the free stream speed of the wind tunnel. The mean chord Reynolds number of the wing is 70,600. Active flow control occurs along the leading edge of the airfoil, which contains 16 spatially localized micro-valve actuators. Details of the experimental setup, a quasi steady state lift model and results involving open-loop proof of concept validation are provided in Part I of this paper. Here we outline principles and considerations associated with close loop design that will be discussed in our talk.
AB - Active flow control has been demonstrated in Part I of this article to modify the lift, drag and pitching moments on a semi-circular wing during "gusting" flow conditions. The low aspect ratio wing, AR = 2.54, is mounted on a captive trajectory system that responds to the instantaneous lift force and pitching moment and the "gusting" flow is simulated by a 0.2 Hz oscillation of the free stream speed of the wind tunnel. The mean chord Reynolds number of the wing is 70,600. Active flow control occurs along the leading edge of the airfoil, which contains 16 spatially localized micro-valve actuators. Details of the experimental setup, a quasi steady state lift model and results involving open-loop proof of concept validation are provided in Part I of this paper. Here we outline principles and considerations associated with close loop design that will be discussed in our talk.
UR - http://www.scopus.com/inward/record.url?scp=78049510216&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=78049510216&partnerID=8YFLogxK
U2 - 10.2514/6.2008-3977
DO - 10.2514/6.2008-3977
M3 - Conference contribution
AN - SCOPUS:78049510216
SN - 9781563479427
T3 - 38th AIAA Fluid Dynamics Conference and Exhibit
BT - 38th AIAA Fluid Dynamics Conference and Exhibit
PB - American Institute of Aeronautics and Astronautics Inc.
ER -