Surface Measurements – Flow Field Correlations Resulting in Applicable Cavity Flow Field Control

Award Information
Agency:
Department of Defense
Branch:
Air Force
Amount:
$99,957.00
Award Year:
2006
Program:
SBIR
Phase:
Phase I
Contract:
FA8650-06-M-3650
Agency Tracking Number:
F061-243-1432
Solicitation Year:
2006
Solicitation Topic Code:
AF06-243
Solicitation Number:
2006.1
Small Business Information
COMBUSTION RESEARCH AND FLOW TECHNOLOGY,
6210 Keller's Church Road, Pipersville, PA, 18947
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
929950012
Principal Investigator
 Srinivasan Arunajatesan
 Senior Research Scientist
 (215) 766-1520
 ajs@craft-tech.com
Business Contact
 Neeraj Sinha
Title: Vice President & Technical Director
Phone: (215) 766-1520
Email: sinha@craft-tech.com
Research Institution
N/A
Abstract
Development of a surface measurements based active feedback flow control strategy for cavity flow fields is proposed. The method relies on the estimation of flow field characteristics using surface pressure measurement. The estimated flow field will be used by a controller to provide suitable actuation to the flow filed to effect control. The actuation requirements will be identified through analysis of existing datasets (computational and experimental). A numerical test bed will be implemented to test this overall strategy and to identify controller requirements. The Phase I part of the program will explore development and refinement of a lower dynamical model, exploration of existing datasets to identify actuation requirements and feasibility testing on a numerical test bed. Phase II part of the program will refine/develop actuators, address controller design and conduct experimental testing at a suitable scale. It is envisioned that the successful completion of this effort will not only achieve a better understanding of the complex phenomenon of flow induced cavity oscillations with and without control, but also result in the development of technology applicable to store separation from internal weapons bays at supersonic speeds.

* information listed above is at the time of submission.

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