Infrared laser absorption thermometry and CO sensing in high-pressure rocket combustion flows from 25 to 105 bar
Author:
Affiliation:
1. University of California, Los Angeles
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1610
Reference18 articles.
1. Infrared laser-absorption sensing for combustion gases
2. Wavelength modulation spectroscopy near 5 $$\upmu$$m for carbon monoxide sensing in a high-pressure kerosene-fueled liquid rocket combustor
3. Laser Absorption Spectroscopy of Carbon Monoxide near 4.97 μm for Temperature and Species Measurements in Hydrocarbon-Fueled Rockets
4. Spectroscopy and Optical Diagnostics for Gases
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