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Spatially Resolved Temperature and Water Vapor Concentration Distributions in Supersonic Combustion Facilities by TDLATDetailed knowledge of the internal structure of high-enthalpy flows can provide valuable insight to the performance of scramjet combustors. Tunable Diode Laser Absorption Spectroscopy (TDLAS) is often employed to measure temperature and species concentration. However, TDLAS is a path-integrated line-of-sight (LOS) measurement, and thus does not produce spatially resolved distributions. Tunable Diode Laser Absorption Tomography (TDLAT) is a non-intrusive measurement technique for determining two-dimensional spatially resolved distributions of temperature and species concentration in high enthalpy flows. TDLAT combines TDLAS with tomographic image reconstruction. More than 2500 separate line-of-sight TDLAS measurements are analyzed in order to produce highly resolved temperature and species concentration distributions. Measurements have been collected at the University of Virginia's Supersonic Combustion Facility (UVaSCF) as well as at the NASA Langley Direct-Connect Supersonic Combustion Test Facility (DCSCTF). Due to the UVaSCF s unique electrical heating and ability for vitiate addition, measurements collected at the UVaSCF are presented as a calibration of the technique. Measurements collected at the DCSCTF required significant modifications to system hardware and software designs due to its larger measurement area and shorter test duration. Tomographic temperature and water vapor concentration distributions are presented from experimentation on the UVaSCF operating at a high temperature non-reacting case for water vitiation level of 12%. Initial LOS measurements from the NASA Langley DCSCTF operating at an equivalence ratio of 0.5 are also presented. Results show the capability of TDLAT to adapt to several experimental setups and test parameters.
Document ID
20130001729
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Busa, K. M.
(Virginia Univ. Charlottesville, VA, United States)
McDaniel J. C.
(Virginia Univ. Charlottesville, VA, United States)
Diskin, G. S.
(NASA Langley Research Center Hampton, VA, United States)
DePiro, M. J.
(NASA Langley Research Center Hampton, VA, United States)
Capriotti, D. P.
(NASA Langley Research Center Hampton, VA, United States)
Gaffney, R. L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 27, 2013
Publication Date
December 3, 2012
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NF1676L-15788
Report Number: NF1676L-15788
Meeting Information
Meeting: 33rd Exhaust Plume and Signatures
Location: Monterey, CA
Country: United States
Start Date: December 3, 2012
End Date: December 7, 2012
Sponsors: Department of the Air Force, NASA Headquarters, Department of the Navy, Department of the Army
Funding Number(s)
CONTRACT_GRANT: FA9550-09-1-0611
CONTRACT_GRANT: NNL11AB32P
WBS: WBS 475122.02.07.09.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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