Near Surface Flow Control Using Magnetohydrodynamics in High Mach Number Flight

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$99,995.00
Award Year:
2005
Program:
STTR
Phase:
Phase I
Contract:
FA9550-05-C-0151
Award Id:
73385
Agency Tracking Number:
F054-016-0045
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
1900 Bates Ave., Suite G, Concord, CA, 94520
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
149397015
Principal Investigator:
Mike McFarland
Principal Scientist
(925) 798-5770
mcfarland@acreetech.com
Business Contact:
Jochen Schein
Vice President
(925) 798-5770
schein@acreetech.com
Research Institution:
WRIGHT STATE UNIV.
James Menart
Department of Mechanical Eng., 3640 Colonel Glenn Hwy.
Dayton, OH, 45435
(937) 775-5154
Nonprofit college or university
Abstract
The purpose of this project is to demonstrate the effectiveness of a Cathodic Arc Plasma Sources (CAPS) and Power Processing Unit (PPU) for producing dense, high current (> 1 amp) plasma flows for magnetohydrodynamic (MHD) control of hypersonic flight surfaces. The CAPS source and PPU were developed for aerospace applications and have been optimized for weight and efficiency. The main advantage of the CAPS sources is that the plasma is generated independently of the current flow, and because of this, high-density, diffuse plasmas with large currents are possible. To characterize the effectiveness of the CAPS plasma source and measure the MHD effects, it will be installed into a model wing section and tested in a hypersonic (Mach 5.1) wind tunnel. The performance, efficiency, power consumption, power/weight ratio, and optimum velocity and altitude range will be determined under flight conditions. In addition, finite element computer simulations will be performed and compared to the experiment results.

* information listed above is at the time of submission.

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