TY - GEN
T1 - Identifying dynamic modes of separated flow subject to ZNMF-based control from surface pressure measurements
AU - Deem, Eric
AU - Cattafesta, Louis
AU - Zhang, Hao
AU - Rowley, Clarence
AU - Hemati, Maziar
AU - Cadieux, Francois
AU - Mittal, Rajat
N1 - Publisher Copyright:
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2017
Y1 - 2017
N2 - Fluid systems are most efficient for fully attached flows, and designers therefore seek to avoid flow separation. Active flow control can help achieve this goal, and closed-loop control offers improved performance at off-design conditions. However, this requires feedback of accurate state estimates to the controller in real time. This motivates a physics-based, state-estimation technique that economically extracts key dynamical features of the flow. This work aims to extract dynamical characteristics of a laminar separation bubble on a flat plate at a chord Reynolds number of 105 using a linear array of unsteady surface pressure measurements. First, DynamicMode Decomposition (DMD) is employed on high-dimensional time-resolved PIV velocity and corresponding estimated pressure fields to identify the dynamically relevant spatial structure and temporal characteristics of the separated flow. Then, results are presented of various open-loop control cases using pulse-modulation of a zero-net mass-flux actuator slot located just upstream of separation. Real-time estimates of the dynamical characteristics are provided by performing on- line DMD onmeasurements froma linear array of 13 unsteady surface pressure transducers. The results show that this method provides reliable estimates of the modal characteristics of the sep- arated flow subject to forcing at a rate much faster than the characteristic time scales of the flow. Therefore, online DMD applied to the surface pressure measurements provides a time-varying linear estimate of the evolution of the controlled flow, thereby enabling closed-loop control.
AB - Fluid systems are most efficient for fully attached flows, and designers therefore seek to avoid flow separation. Active flow control can help achieve this goal, and closed-loop control offers improved performance at off-design conditions. However, this requires feedback of accurate state estimates to the controller in real time. This motivates a physics-based, state-estimation technique that economically extracts key dynamical features of the flow. This work aims to extract dynamical characteristics of a laminar separation bubble on a flat plate at a chord Reynolds number of 105 using a linear array of unsteady surface pressure measurements. First, DynamicMode Decomposition (DMD) is employed on high-dimensional time-resolved PIV velocity and corresponding estimated pressure fields to identify the dynamically relevant spatial structure and temporal characteristics of the separated flow. Then, results are presented of various open-loop control cases using pulse-modulation of a zero-net mass-flux actuator slot located just upstream of separation. Real-time estimates of the dynamical characteristics are provided by performing on- line DMD onmeasurements froma linear array of 13 unsteady surface pressure transducers. The results show that this method provides reliable estimates of the modal characteristics of the sep- arated flow subject to forcing at a rate much faster than the characteristic time scales of the flow. Therefore, online DMD applied to the surface pressure measurements provides a time-varying linear estimate of the evolution of the controlled flow, thereby enabling closed-loop control.
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U2 - 10.2514/6.2017-3309
DO - 10.2514/6.2017-3309
M3 - Conference contribution
AN - SCOPUS:85088201660
SN - 9781624105005
T3 - 47th AIAA Fluid Dynamics Conference, 2017
BT - 47th AIAA Fluid Dynamics Conference, 2017
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 47th AIAA Fluid Dynamics Conference, 2017
Y2 - 5 June 2017 through 9 June 2017
ER -