In this project, methods of model reduction that integrate feedback active flow control with applications to nonlinear convection and turbulent flows governed by Navier-Stokes equations are developed. A new methodology which extracts boundary conditions in reduced order proper orthogonal decomposition (POD) and finite difference models is developed. A new model reduction method based on empirical data and balanced truncation was developed and applied to nonlinear Galerkin models. Based on this method a new empirical Hankel norm model reduction algorithm is proposed. These methods are applied to a prototype nonlinear convective problem governed by the two-dimensional (2D) Burgers' equation. The reduced models are used in the design of robust boundary controllers that achieve tracking, and implemented on the full order Computational Fluid Dynamics (CFD) models. POD and balanced truncation are shown to be optimal in the sense of distance minimizations in spaces of Hilbert-Schmidt (HS) operators. POD has been shown to be optimal in a broader sense than is reported in the literature. The optimality is in the sense of distance minimization in a space of integral operators under the Hilbert-Schmidt norm. A connection with balanced truncation is found. In particular, balanced truncation is shown to be optimal in the sense of distance minimization albeit in a different space of integral operators under the Hilbert-Schmidt norm when the so-called 'Curtain-Glover' balanced realization is used. This is a novel discovery as balanced truncation is usually known to be not optimal in any sense.An algorithm that combines the extended Kalman filter and expectation maximization to estimate the model coefficients from particle image velocimetry (PIV) measurements for turbulent 2D flows is developed. The algorithm is recursive and convenient for on-line implementation. The method is applied to a 2D flow control problem over the NACA 4412 airfoil using experimental data obtained from Prof. Glauser's flow control group at the University of Syracuse. The motivation for this problem is minimization of aero-optic distortion in a bluff-body flow.POD and balanced truncation are shown to minimize different n-widths of partial differential equation solutions including the Kolmogorov, Gelfand, linear and Bernstein n-widths. The nwidths are notions from metric complexity theory. They quantify inherent and representation errors due to lack of data and loss of information.
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