Enhanced Dielectric Barrier Discharge Devices for Active Control of Flow Separation

Award Information
Agency:
Department of Defense
Branch
Navy
Amount:
$69,874.00
Award Year:
2010
Program:
SBIR
Phase:
Phase I
Contract:
N00014-09-M-0466
Agency Tracking Number:
N092-144-0495
Solicitation Year:
2009
Solicitation Topic Code:
N092-144
Solicitation Number:
2009.2
Small Business Information
Creare Inc.
P.O. Box 71, Hanover, NH, 03755
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
072021041
Principal Investigator:
Richard Kaszeta
Principal Investigator
(603) 643-3800
rwk@creare.com
Business Contact:
James Barry
President
(603) 643-3800
contractsmgr@creare.com
Research Institution:
n/a
Abstract
One of the most important factors in improving aerodynamic performance of aircraft is the ability to control flow separation from lift and control surfaces. On many military aircraft, passive vortex generators are currently used to create high levels of vorticity along control and lift surfaces, but these are purely passive devices, and it would be more advantageous to create controllable levels of body force, turbulence, and vorticity to improve overall aerodynamic performance. What is needed is a practical technique for active flow control. Surface-mounted Dielectric Barrier Discharge (DBD) plasma actuators have been studied in several laboratories, and they are a potentially attractive approach to achieve active flow control. Creare, in cooperation with the University of Minnesota, proposes to develop an active transition and drag reduction control system based upon wing-mounted DBDs using asymmetric thrust generation to improve DBD performance. We will develop a system that is practical for actual aircraft application. The system will be characterized, packaged appropriately for aircraft installation, and made robust enough to both survive and function in real-world military scenarios.

* information listed above is at the time of submission.

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