Abstract
This study demonstrates the applicability of 2D species visualization inside a gas turbine combustor using larer-induced fluorescence (LIF). Time-averaged and single-shot OH and NO distributions were analyzed to clarify the characteristics of the NO formation inside the combustor. The turbulent flame front was clearly seen using single-shot OH measurement to elucidate the burning pattern in the combustor. It became clear that NO was mainly produced near the pilot burner and that it tended to exist at the center of the combustor.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callMore From: TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
