Simultaneous 100-kHz acetone planar laser-induced fluorescence and OH* chemiluminescence in a linear non-premixed detonation channel

Ayers, Zachary M.; Lemcherfi, Aaron; Plaehn, Ethan W.; Gejji, Rohan; Perkins, H. Douglas; Roy, Sukesh; Slabaugh, Carson D.; Meyer, Terrence R.; Fugger, Christopher A.

doi:10.1016/j.combustflame.2022.112209

Cited by 19 publications

(1 citation statement)

References 57 publications

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“…In such simulations, burnt gases are not taken into account. A cold-flow simulation can give insight for a preliminary characterization of the injection system efficiency, but it cannot capture some important effects such as axial stratification of fuel and oxidizer in an operating RDC, obtained in simulations by Gaillard et al (2017), and in experiments by Ayers et al (2022). Such stratification is mainly due to the asynchronous recovery of the fuel and oxidizer flows after the passage of a detonation wave followed by the burnt gas expansion.…”

Section: Introductionmentioning

confidence: 99%

Evaluation of a computational strategy to model transitory injection in rotating detonation combustors

Hellard

Gaillard²,

Davidenko³

2023

Front. Aerosp. Eng.

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The efficiency of a Rotating Detonation Combustor (RDC) strongly depends on the transitory injection process of fresh reactants in the combustion chamber: poor propellant mixing induces losses of combustion efficiency and consequently low detonation speed and unstable detonation propagation. Moreover, dilution of fresh reactants with burnt gases during injection increases the deflagration losses and decreases the pressure gain provided by the detonation. Numerical simulation can help design an efficient injector to reduce these losses. In this study, the modeling strategy previously proposed by ONERA to simulate the transitory injection process is applied to two existing experimental RDC (from Nagoya University and TU Berlin) and one in-development RDC from ONERA. The computational domain represents only one injection element, convenient for a parametric study at low computational cost. A custom initial condition is used to model the expansion process of burnt gases past a detonation wave. The initial condition parameters are discussed and a method is proposed to correctly set them. The TU Berlin RDC is studied in more detail: mixing efficiency up to 70% is obtained, and 5% of deflagration losses are estimated according to the assumptions of the simulation. Based on the numerical results, detonation speed was evaluated at various distances from the injection plane taking into account the heterogeneities of the fresh mixture. The measured speed lies within the predicted range.

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Section: Introductionmentioning

confidence: 99%