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Towards Simultaneous Multi-Parameter Measurements Using Burst-Mode Frequency-Scanning Planar Laser-Induced FluorescenceWhile planar laser-induced fluorescence (PLIF) can provide valuable flow visualization, there are many challenges in extracting quantitative measurements from the fluorescence intensity. To overcome the multi-parameter dependence of the signal intensity, frequency scanning planar laser-induced fluorescence (FS-PLIF) provides the potential for 2D temperature, pressure, and velocity measurements by spectrally resolving the excitation spectrum of one or more fluorescence transitions to extract the Doppler shift, Doppler- and collisional-broadening of absorption lines, and the relative signal intensities of multiple transitions. This work aims to characterize a burst-mode FS-PLIF system consisting of a Spectral Energies, LLC burst-mode laser coupled with a Spectral Energies, LLC optical parametric oscillator using nitric oxide (NO) static pressure cell measurements. The effect of the OPO cavity on intensity fluctuations during frequency-scanning is investigated. A NO PLIF model is implemented to investigate the feasibility of property measurements using single- and two-NO-line scans.
Document ID
20240014904
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Amanda M Braun
(Oak Ridge Associated Universities Oak Ridge, United States)
Neil S Rodrigues
(Langley Research Center Hampton, United States)
Paul M Danehy
(Langley Research Center Hampton, United States)
Date Acquired
November 21, 2024
Subject Category
Instrumentation and Photography
Meeting Information
Meeting: AIAA Scitech Forum and Exposition
Location: Orlando, FL
Country: US
Start Date: January 6, 2025
End Date: January 10, 2025
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 335803.04.22.23.10.01
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
Keywords
burst-mode laser
planar laser-induced fluorescence
pressure
temperature
velocity
hypersonics
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