On the role of transverse detonation waves in the re-establishment of attenuated detonations in methane-oxygen

被引:19
作者
Floring, Grace [1 ]
Peswani, Mohnish [1 ]
Maxwell, Brian [1 ]
机构
[1] Case Western Reserve Univ, Dept Mech & Aerosp Engn, 10900 Euclid Ave,Glennan 418, Cleveland, OH 44106 USA
关键词
Compressible flows; Detonation waves; Critical re-initiation; Four step combustion; Numerical simulation; Transverse detonations; RESOLUTION NUMERICAL-SIMULATION; MACH REFLECTION; RE-INITIATION; DIFFRACTION; DEFLAGRATION; MECHANISM; TRANSITION;
D O I
10.1016/j.combustflame.2022.112497
中图分类号
O414.1 [热力学];
学科分类号
摘要
This investigation concerns the problem of detonation attenuation in stoichiometric methane-oxygen and its re-establishment following its interaction with obstacles, using high resolution numerical simulation. The main focus was on the role of the transverse detonation on the re-establishment of the detonation wave, and the importance of applying a numerical combustion model that responds appropriately to the thermodynamic state behind the complex shock wave dynamics. We applied an efficient thermochemi-cally derived four-step global combustion model using an Euler simulation framework to investigate the critical regimes present. While past attempts at using one-or two-step models have failed to capture transverse detonations, for this scenario, our simulations have demonstrated that the four-step combus-tion model is able to capture this feature. We thus suggest that to correctly model detonation re-initiation in characteristically unstable mixtures, an applied combustion model should contain at least an adequate description to permit the correct ignition and state variable response when changes in temperature and pressure occur, i.e., behind shocks. Our simulations reveal that (1) there is a relationship between the critical outcomes possible and the mixture cell size, and (2) while pockets of unburned gas may exist when a detonation re-initiates, it is not the direct rapid consumption of these pockets that gives rise to transverse detonations. Instead, the transverse detonations are initiated through pressure amplification of reaction zones at burned/unburned gas interfaces whose combustion rates have been enhanced through Richtmyer-Meshkov instabilities associated with the passing of transverse shock waves, or by sponta-neous ignition of hot spots, which can form into detonations through the Zeldovich gradient mechanism. In both situations, non-uniform ignition delay times are found to play a role. Finally, we found that the transverse detonations are in fact Chapman-Jouguet detonations, but whose presence contributes to over-driving the re-initiated detonation along the Mach stem.(c) 2022 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
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页数:23
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