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Detonation propagation across a stratified layer with a diffuse interface

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TLDR
In this article, a study was conducted to examine detonation propagation in a stratified layer of hydrogen-oxygen-nitrogen above an inert gas in a horizontal narrow channel.
Abstract
A study was conducted to examine detonation propagation in a stratified layer of hydrogen-oxygen-nitrogen above an inert gas in a horizontal narrow channel. The stratified layer was produced by a gravity current, generated by retracting a door initially separating a hydrogen-oxygen-nitrogen mixture in the predetonator and a heavier inert gas in the test-section. A steady detonation wave generated in the predetonator was transmitted into the stratified layer. The reactivity of the predetonator mixture was varied via the hydrogen-oxygen equivalence ratio and the amount of nitrogen dilution. Schlieren photography was used to visualize the detonation front in the test-section, and soot foils were used to obtain the cellular structure. Schlieren imaging showed a curved detonation front that decoupled at about mid channel height, into a shock wave and trailing contact surface. Both the hydrogen-oxygen-nitrogen reactivity and the type of inert gas initially in the test-section affected the distance travelled by the detonation wave in the stratified layer. The mixture composition distribution within the test-section before ignition was obtained via a three-dimensional CFD simulation. The lateral extent of the cellular structure captured on the soot foil, coincided with the calculated inert gas mole fraction contour that corresponds to a sharp increase in the ZND induction zone length, e.g., 70% argon dilution for a stoichiometric hydrogen-oxygen predetonator mixture.

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Experimental visualization of sphere-induced oblique detonation in a non-uniform mixture

TL;DR: In this paper , a stratified H2/O2-3Ar mixture was supplied with a concentration gradient normal to the launching direction of a two-stage light gas gun, and high-speed schlieren images were taken to study the morphologies of oblique detonation.
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Experimental observation on the end-gas autoignition and detonation affected by chemical reactivity in confined space

TL;DR: In this paper , the effect of the chemical reactivity of different fuels and diluent gases on the end-gas autoignition and detonation development in a confined space was investigated.
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A flame technique to isolate the detonation/product interface relevant to rotating detonation engines

TL;DR: In this paper , a novel experimental technique is proposed to study the detonation propagation in a layer of non-reacted gas weakly confined by combustion products, which is relevant to rotating detonation engines, where transverse detonations are confined by products of a previous rotation cycle, and other applications such as industrial safety.
References
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Journal ArticleDOI

Gravity currents and related phenomena

TL;DR: In this paper, the authors present a broad investigation into the properties of steady gravity currents, in so far as they can be represented by perfect-fluid theory and simple extensions of it (like the classical theory of hydraulic jumps) that give a rudimentary account of dissipation.
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Flame acceleration and transition to detonation in ducts

TL;DR: In this article, the state of knowledge on flame acceleration and deflagration-to-detonation transition (DDT) in smooth ducts and ducts equipped with turbulence-producing obstacles is reviewed.
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Rotating detonation combustors and their similarities to rocket instabilities

TL;DR: An overview of the research done worldwide to address some of the challenges and questions pertaining to the physics of rotating detonation combustors operation is provided in this paper, where notable parallels are drawn to the phenomena of low and high frequency instabilities in solid and liquid rockets that have been recognized as the most severe hindrance to their operation.
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Detonation diffraction in gases

TL;DR: In this paper, the authors examined how the extent of detonation cellular instability influences the quantitative and qualitative features of diffraction and found that the most striking differences between the mixtures occur in the sub-critical and critical regimes, for which the detonation fails to transition into the unconfined half-space.
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Detonation propagation in hydrogen-air mixtures with transverse concentration gradients

TL;DR: In this paper, the influence of transverse concentration gradients on detonation propagation was investigated experimentally in a wide parameter range, and significant amounts of mixture seem to be consumed by turbulent deflagration behind the leading detonation.
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