Modeling and Control of Turbulent Wall-Bounded Shear Flows
This work introduces new methods for modeling and control of turbulent wall-bounded shear flows. Transition in these flows is crucial to the technologically relevant problem of skin-friction drag reduction. This form of drag results from the no-slip boundary conditions on the surface of a submarine or the fuselage and the wings of an aircraft; it accounts for approximately 50% of the overall drag of a subsonic aircraft at cruise conditions, and approximately 90% of the overall drag of an underwater vehicle. Progress in these problems has been hindered by the lack of understanding of turbulent flows and the absence of tractable models and theoretical tools for analysis and control thereof. Since skin-friction drag directly translates into large fuel consumption for air and water vehicles, there is a critical demand for development and utilization of advanced theoretical and computational techniques in this area. The researchers are developing new control-oriented models of turbulent wall-bounded shear flows; these models will contain appropriate statistical description of flow disturbances that approximate turbulent flow statistics (that will be determined using MSI computational resources) in the least-squares sense. The flow estimators and controllers designed using these models will have superior performance compared to their counterparts designed without an accurate statistical description of flow disturbances. This approach will enable successful skin-friction drag reduction at higher Reynolds numbers than currently possible.
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