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Simultaneous 100-kHz Acetone Planar Laser-Induced Fluorescence and OH* Chemiluminescence in a Linear Non-Premixed Detonation Channel

Authors :
Zachary M Ayers
Aaron Lemcherfi
Ethan W Plaehn
Rohan M Gejji
H Douglas Perkins
Sukesh Roy
Carson D Slabaugh
Terrence R Meyer
Christopher Fugger
Source :
Combustion and Flame. 244
Publication Year :
2022
Publisher :
United States: NASA Center for Aerospace Information (CASI), 2022.

Abstract

Reactant 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.

Subjects

Subjects :
Spacecraft Propulsion And Power

Details

Language :
English
ISSN :
15562921 and 00102180
Volume :
244
Database :
NASA Technical Reports
Journal :
Combustion and Flame
Notes :
264925.04.22.22, , 80NSSC21C0031
Publication Type :
Report
Accession number :
edsnas.20210023359
Document Type :
Report
Full Text :
https://doi.org/10.1016/j.combustflame.2022.112209