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Imaging fluorescent combustion species in gas turbine flame tubes - On complexities in real systems
Author(s) -
Yolanda R. Hicks,
Robert C. Anderson,
M. Zaller,
Randy J. Locke,
Harold Schock
Publication year - 1997
Publication title -
33rd joint propulsion conference and exhibit
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.1997-2837
Subject(s) - combustion , gas turbines , fluorescence , materials science , environmental science , aerospace engineering , mechanical engineering , chemistry , engineering , optics , physics , organic chemistry
Planar laser-induced fluorescence (PLIF) is used to visualize the flame structure via OH, NO, and fuel imaging in kerosine-burning gas turbine combustor flame tubes. When compared to simple gaseous hydrocarbon flames and hydrogen flames, flame tube testing complexities include spectral interferences from large fuel fragments, unknown turbulence interactions, high pressure operation, and the concomitant need for windows and remote operation. Complications of these and other factors as they apply to image analysis are considered. Because both OH and gas turbine engine fuels (commercial and military) can be excited and detected using OH transition lines, anarrowband and abroadband detection scheme are compared and the benefits and draw-backs of each method are examined.

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