Simultaneous Temperature and Velocity Diagnostic for Reacting Flows

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$99,974.00
Award Year:
2011
Program:
SBIR
Phase:
Phase I
Contract:
NNX11CD83P
Award Id:
n/a
Agency Tracking Number:
104427
Solicitation Year:
2010
Solicitation Topic Code:
A2.02
Solicitation Number:
n/a
Small Business Information
CA, Irvine, CA, 92618-2008
Hubzone Owned:
N
Minority Owned:
Y
Woman Owned:
N
Duns:
188465819
Principal Investigator:
ThomasJenkins
Principal Investigator
(949) 553-0688
tjenkins@metrolaserinc.com
Business Contact:
ChristinaArnold
Director of Administration
(949) 553-0688
carnold@metrolaserinc.com
Research Institute:
Stub




Abstract
A diagnostic technique is proposed for measuring temperature and velocity simultaneously in a high temperature reacting flow for aiding research in propulsion. The technique involves seeding particles of a ceramic thermographic phosphor into the flow and illuminating them with two overlapping pulsed laser sheets. Laser-induced luminescence from the particles will be measured to obtain temperature from its effects on luminescence lifetime. Velocity will be obtained simultaneously from the same particles using conventional particle image velocimetry (PIV). Each of the two diagnostics will employ a separate CCD camera that captures a pair of images separated by a short delay. For the thermometry technique, pixel intensity ratios of the delayed to the undelayed images will be related to temperature via a calibration function. In the PIV technique, particle displacements between the images will be obtained using conventional interrogation window techniques with cross-correlation. The proposed diagnostic is expected to enable spatially and temporally correlated measurements of two key variables in combustion modeling that cannot be obtained in most high temperatures flows using currently available methods. The phase I effort will demonstrate feasibility measurements in a flame.

* information listed above is at the time of submission.

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