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Simultaneous 100-kHz Acetone Planar Laser-Induced Fluorescence and OH* Chemiluminescence in a Linear Non-Premixed Detonation ChannelReactant mixing and combustion are investigated in an optically accessible, self-excited linear detonation combustor. The mixing field is captured using 100 kHz planar laser-induced fluorescence (PLIF) imaging of acetone as a tracer in the fuel supply, while 100 kHz chemiluminescence imaging of excited-state hydroxyl (OH*) radicals simultaneously resolves the evolution of the detonation wave. Time sequences are acquired over multiple detonation cycles in each test, with acetone-PLIF images collected along multiple orthogonal planes to reveal the complex three-dimensional topography of the fuel distribution. The instantaneous and phase averaged acetone-PLIF images enable measurement of key fuel injection characteristics, such as the injector recovery time, fuel jet velocity, and refill height for a range of operating conditions. Instantaneous and phase-averaged measurements of acetone-PLIF with the time-coincident OH* chemiluminescence images also reveal a number key features, such as fuel stratification and weak detonation in the injector near field, incomplete combustion and deflagration behind the detonation wave, vitiation and deflagration of reactants ahead of the detonation wave, and fuel and oxidizer recovery time mismatch leading to combustion inefficiency. These measurements significantly enhance the ability to obtain detailed information on the intracycle and intercycle spatiotemporal evolution of the reactant refill process and its coupled effects on the detonation wave structure and propagation.
Document ID
20210023359
Acquisition Source
Glenn Research Center
Document Type
Accepted Manuscript (Version with final changes)
Authors
Zachary M Ayers
(Purdue University West Lafayette West Lafayette, Indiana, United States)
Aaron Lemcherfi
(Purdue University West Lafayette West Lafayette, Indiana, United States)
Ethan W Plaehn
(Purdue University West Lafayette West Lafayette, Indiana, United States)
Rohan M Gejji
(Purdue University West Lafayette West Lafayette, Indiana, United States)
H Douglas Perkins
(Glenn Research Center Cleveland, Ohio, United States)
Sukesh Roy
(Spectral Energies (United States) Dayton, Ohio, United States)
Carson D Slabaugh
(Purdue University West Lafayette West Lafayette, Indiana, United States)
Terrence R Meyer
(Purdue University West Lafayette West Lafayette, Indiana, United States)
Christopher Fugger
(Spectral Energies (United States) Dayton, Ohio, United States)
Date Acquired
October 25, 2021
Publication Date
June 13, 2022
Publication Information
Publication: Combustion and Flame
Publisher: Elsevier
Volume: 244
Issue Publication Date: October 1, 2022
ISSN: 0010-2180
e-ISSN: 1556-2921
Subject Category
Spacecraft Propulsion And Power
Funding Number(s)
WBS: 264925.04.22.22
CONTRACT_GRANT: 80NSSC21C0031
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Propulsion
Rocket
Detonation
Instrumentation
Diagnostics
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