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Proceedings Paper

Optical measurement and visualization in high-pressure high-temperature aviation gas turbine combustors
Author(s): Yolanda R. Hicks; Randy J. Locke; Robert C. Anderson
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Paper Abstract

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.

Paper Details

Date Published: 31 August 2000
PDF: 12 pages
Proc. SPIE 4076, Optical Diagnostics for Industrial Applications, (31 August 2000); doi: 10.1117/12.397964
Show Author Affiliations
Yolanda R. Hicks, NASA Glenn Research Ctr. (United States)
Randy J. Locke, Dynacs Engineering Co. (United States)
Robert C. Anderson, NASA Glenn Research Ctr. (United States)


Published in SPIE Proceedings Vol. 4076:
Optical Diagnostics for Industrial Applications
Neil A. Halliwell, Editor(s)

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