Computational Methods for Feedback Flow Controllers in Aerodynamic Applications

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: F49620-03-C-0092
Agency Tracking Number: F033-0051
Amount: $99,996.00
Phase: Phase I
Program: STTR
Awards Year: 2003
Solicitation Year: N/A
Solicitation Topic Code: N/A
Solicitation Number: N/A
Small Business Information
PO Box 233, 663 Owego Hill Road, Harford, NY, 13784
DUNS: 037658379
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Henry Carlson
 (607) 844-9171
Business Contact
 Henry Carlson
Title: President
Phone: (607) 844-9171
Research Institution
 Jeanne De Pass
 10920 Wilshire Blvd., Suite 1200
Los Angeles, CA, 90024
 (310) 794-0135
 Nonprofit college or university
Clear Science Corp. and the University of California at Los Angeles propose to develop a versatile and comprehensive computational toolbox for designing feedback flow controllers in aerodynamic applications. Target objectives include separation control tomanage lift and form drag, control of transition to turbulence, turbulence control to reduce skin friction drag, increase mixing, or reduce heat transfer, and control of acoustical output (noise suppression). The toolbox will be modular withinterchangeable reduced-order modeling algorithms, system state estimators, and controller designs. We will leverage our team''s work in low-dimensional modeling, balanced order reduction, stochastic estimators, standard controllers for linear systems,and advanced modeling for nonlinear systems. Phase I objectives include demonstrating a prototype of the computational toolbox. The proof-of-concept prototype will target several feedback flow control applications involving different computationaldomains, flow conditions, and control input-output. Reduced-order models, estimators, and controllers will be designed for each application. A second objective is formulation of a Phase II development and test plan. The Phase II plan will includedevelopment of libraries of reduced-order models, estimators, and controllers for feedback flow control. Tests will consist of CFD, controller-in-the-loop simulations to demonstrate modeling and estimation accuracy, controller robustness, and interfacingbetween the computational toolbox and third-party software. The commercial product to be developed is a validated computational toolbox for designing feedback flow controllers in aerospace and industrial applications. The corresponding market includesdesigners of aerospace, automotive, and industrial systems for which flow control is critical. Potential applications of the software include control system designs for low-drag wings on commercial aircraft, low-drag bodies in high-performance automobiles,high-lift blades in rotorcraft, low-distortion jet engine inlets, and high-mixing combustors. Interfaces between the feedback flow control toolbox, commercial CFD codes, and software like Matlab will provide the conduit for commercialization, enablingengineers to incorporate flow control into the overall design process, perform control-in-the-loop simulations, and utilize standard controller designs.

* Information listed above is at the time of submission. *

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