![]() ![]() ![]() ![]() Integral to the POD/mLSE algorithm is the estimation of the global POD coefficients. From such estimates knowledge of the state of the flow above the airfoil can be obtained (i.e., attached, fully separated or incipiently separated). By using a combination of Particle Image Velocimetry PIV and multiple surface pressure measurements, processed through a POD/mLSE algorithm, estimates of the velocity field from wall pressure alone are extracted. N2 - We are developing feedback control methods based on the use of Proper Orthogonal Decomposition POD and Modified Linear Stochastic Estimation mLSE for the flow over a NACA 4412 airfoil. T1 - POD based experimental flow control on a NACA-4412 airfoil (invited) ![]()
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