Methane Oxidation Rates at Turbine-Relevant Conditions in a High Pressure Catalytic Shock Tube

JJ Urso, C Kinney, M Pierro, CW Dennis… - AIAA SCITECH 2023 …, 2023 - arc.aiaa.org
JJ Urso, C Kinney, M Pierro, CW Dennis, J McGaunn, C Mills, S Vasu
AIAA SCITECH 2023 Forum, 2023arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-0498. vid Stoichiometric oxy-
methane mixtures at pressures of 18.9 to 24 bar and temperatures between 1178–1642 K
were studied in a shock tube. Emission spectroscopy, laser Schlieren, pressure histories,
and fixed wavelength laser absorption spectroscopy at 3.39 μm has been used to measure
methane decomposition rates and find the absorption cross-section of methane at 3.39 μm
at these conditions. Various catalytic end walls were employed to determine any surface …
View Video Presentation: https://doi.org/10.2514/6.2023-0498.vid
Stoichiometric oxy-methane mixtures at pressures of 18.9 to 24 bar and temperatures between 1178 – 1642 K were studied in a shock tube. Emission spectroscopy, laser Schlieren, pressure histories, and fixed wavelength laser absorption spectroscopy at 3.39 μm has been used to measure methane decomposition rates and find the absorption cross-section of methane at 3.39 μm at these conditions. Various catalytic end walls were employed to determine any surface effects caused by the catalytic material observable at a location remote from the end wall.
AIAA Aerospace Research Center
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