Paper
31 August 2000 Optical measurement and visualization in high-pressure high-temperature aviation gas turbine combustors
Yolanda R. Hicks, Randy J. Locke, Robert C. Anderson
Author Affiliations +
Proceedings Volume 4076, Optical Diagnostics for Industrial Applications; (2000) https://doi.org/10.1117/12.397964
Event: Symposium on Applied Photonics, 2000, Glasgow, United Kingdom
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.
© (2000) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Yolanda R. Hicks, Randy J. Locke, and Robert C. Anderson "Optical measurement and visualization in high-pressure high-temperature aviation gas turbine combustors", Proc. SPIE 4076, Optical Diagnostics for Industrial Applications, (31 August 2000); https://doi.org/10.1117/12.397964
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Cited by 32 scholarly publications.
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KEYWORDS
Combustion

Cameras

Mie scattering

Visualization

Raman spectroscopy

Chemiluminescence

Spectroscopy

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