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CARS Temperature and Species Concentration Measurements in a Supersonic Combustor with Normal InjectionThe dual-pump coherent anti-Stokes Raman spectroscopy (CARS) method was used to measure temperature and the absolute mole fractions of N2, O2 and H2 in a supersonic combustor. Experiments were conducted in the NASA Langley Direct-Connect Supersonic Combustion Test Facility. CARS measurements were performed at the facility nozzle exit and at three planes downstream of fuel injection. Processing the CARS measurements produced maps of the mean temperature, as well as quantitative N2 and O2 and qualitative H2 mean mole fraction fields at each plane. The CARS measurements were also used to compute correlations between fluctuations of the different simultaneously measured parameters. Comparisons were made between this 90 degree angle fuel injection case and a 30 degree fuel injection case previously presented at the 2004 Reno AIAA Meeting.
Document ID
20050042046
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Tedder, S. A.
(NASA Langley Research Center Hampton, VA, United States)
OByrne, S.
(New South Wales Univ. Canberra, Australia)
Danehy, P. M.
(NASA Langley Research Center Hampton, VA, United States)
Cutler, A. D.
(George Washington Univ. Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Subject Category
Inorganic, Organic And Physical Chemistry
Report/Patent Number
AIAA Paper 2005-0616
Report Number: AIAA Paper 2005-0616
Meeting Information
Meeting: 43rd Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 10, 2005
End Date: January 13, 2005
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available