4.6 Article

Time-resolved, single-ended laser absorption thermometry and H2O, CO2, and CO speciation in a H2/C2H4-fueled rotating detonation engine

Journal

PROCEEDINGS OF THE COMBUSTION INSTITUTE
Volume 38, Issue 1, Pages 1719-1727

Publisher

ELSEVIER SCIENCE INC
DOI: 10.1016/j.proci.2020.06.125

Keywords

Laser absorption spectroscopy; Rotating detonation engine; Wavelength modulation spectroscopy

Funding

  1. Office of Naval Research
  2. Innovative Scientific Solution, Inc. [N00014-15-P-1121]
  3. Department of Defense through the National Defense Science and Engineering Graduate (NDSEG) Fellowship

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Rotating detonation engines (RDEs) require novel diagnostic tools for better understanding complex detonation behavior and improving performance. A single-ended laser absorption sensor has been developed and deployed for in situ, time-resolved measurements of temperature and gas species concentrations in the annulus of a hydrogen/ethylene/air-fed RDE. With a measurement rate of 44 kS/s, the sensor can provide high-quality data for gas temperature and species.
Rotating detonation engines (RDEs) require novel diagnostic tools to better understand complex detonation behavior and improve performance. To this end, a single-ended laser absorption sensor for in situ , time-resolved measurements of temperature, H2O, CO2, and CO concentrations has been developed and deployed within the annulus of a hydrogen/ethylene/air-fed RDE. With a measurement rate of 44 kS/s, the sensor delivers four co-aligned, mid-infrared laser beams into the annular detonation chamber and captures the back-reflected radiation through a single optical port. A ray-tracing optimization algorithm, designed to maximize signal-to-noise ratio and beam-perturbation tolerance, was used to determine the optimal sensor optical configuration. Wavelength-modulation spectroscopy (WMS) further compensated for interference sources in the harsh detonation environment. Time-resolved and time-averaged sensor measurements of gas temperature and species at equivalence ratios of 0.74, 0.87, and 1.03 are presented. (C) 2020 The Combustion Institute. Published by Elsevier Inc. All rights reserved.

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