NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Optical Measurement and Visualization in High-Pressure, High-Temperature, Aviation Gas Turbine CombustorsPlanar 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.
Document ID
20000121255
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Hicks, Yolanda R. (NASA Glenn Research Center Cleveland, OH United States)
Anderson, Robert C. (NASA Glenn Research Center Cleveland, OH United States)
Locke, Randy J. (DYNACS Engineering Co., Inc. Brook Park, OH United States)
Date Acquired
September 7, 2013
Publication Date
September 1, 2000
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:210377
NASA/TM-2000-210377
E-12431
Meeting Information
Meeting: EOS/SPIE Symposium on Applied Photonics
Location: Glasgow, Scotland
Country: United Kingdom
Start Date: May 22, 2000
End Date: May 25, 2000
Sponsors: European Optical Society, International Society for Optical Engineering
Funding Number(s)
PROJECT: RTOP 714-02-40
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available