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Optical Measurement and Visualization in High-Pressure, High-Temperature, Aviation Gas Turbine Combustors

Author
Hicks, Yolanda R.
Published
September 2000.
Physical Description
1 electronic document
Additional Creators
Locke, Randy J. and Anderson, Robert C.
Online Version

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Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Planar laser-induced fluorescence (PLIF), planar Mie scattering (PMie), and linear (1-D) spontaneous Raman scattering are applied to flame tube and sector combustors that burn Jet-A fuel at a range of inlet temperatures and pressures that simulate conditions expected in future high-performance civilian gas turbine engines. Chemiluminescence arising from C2 in the flame was also imaged. Flame spectral emissions measurements were obtained using a scanning spectrometer. Several different advanced concept fuel injectors were examined. First-ever PLIF and chemiluminescence data are presented from the 60-atm Gas turbine combustor facility.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 20000121255.
NASA/TM-2000-210377.
NAS 1.15:210377.
E-12431.
EOS/SPIE Symposium on Applied Photonics; 22-25 May 2000; Glasgow, Scotland; United Kingdom.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15640313