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Liquid fuel refill dynamics in a rotating detonation combustor using megahertz planar laser-induced fluorescence

  • Matthew W. Hoeper
  • , Austin M. Webb
  • , Venkat Athmanathan
  • , Robert B. Wang
  • , H. Douglas Perkins
  • , Sukesh Roy
  • , Terrence R. Meyer
  • , Christopher A. Fugger

Research output: Contribution to journal › Article › peer-review

Abstract

The highly dynamic response of a continuously injected liquid fuel jet to rotating detonation waves is a critical parameter in the design, performance optimization, and modeling of a rotating detonation engine (RDE). In this work, this response is spatio-temporally resolved from the fuel injection point to the detonation channel using planar laser-induced fluorescence (PLIF) at imaging rates up to 1 MHz. A rotating detonation combustor (RDC) is operated on hydrogen and air to sustain stable detonation waves that interact in a one-way coupled manner with a single liquid fuel jet that propagates into the combustion chamber with cycle periods of ∼250 µs. Diesel is utilized as a realistic fuel surrogate with higher aromatic compounds to enable fluorescence excitation using the 355 nm third-harmonic output of a burst-mode Nd:YAG laser. By optimizing the technique to accommodate orders of magnitude variations in the fuel density throughout the injection process, the PLIF data enable measurements of (i) the overall refill dynamics after the arrival of the detonation wave, (ii) changes in the liquid spray trajectory with microsecond temporal resolution, and (iii) the time required to reestablish the quasi-steady axial refilling process as a function of peak chamber pressure relative to the air- and liquid-injector pressure drops. As the passage of the detonation wave imparts significant changes in the momentum flux ratio, the qualitative liquid break-up process and spatial distribution of the spray also vary significantly in time. Only as the injection system recovers late in the cycle does the fuel spray eventually return to a quasi-steady position and allow comparisons with theoretical jet trajectories. These data, enabled by ultra-high-speed PLIF imaging, represent some of the first detailed measurements for quantifying the dynamic response and recovery of liquid jets exposed to periodic detonations in an operating RDC.

Original languageEnglish (US)
Pages (from-to)3051-3061
Number of pages11
JournalProceedings of the Combustion Institute
Volume39
Issue number3
DOIs
StatePublished - Jan 2023
Externally publishedYes

Bibliographical note

Publisher Copyright:
© 2022 The Combustion Institute

Keywords

  • Fuel spray
  • High-speed imaging
  • Planar laser-induced fluorescence
  • Rotating detonation combustor
  • Rotating detonation engine

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