Reactive transverse waves in a near-limit detonation
Abstract
The reactivity of transverse waves in detonations of methane, oxygen and nitrogen are experimentally assessed using MHz rate schlieren and chemiluminescence imaging. In these highly unstable mixtures, the mode of wave propagation is more complex than what is described by the cellular instability model that is conventionally used for weakly unstable mixtures. Behind the low-speed leading shock in unstable waves, the processed gas remains essentially unreacted until transverse waves reach this region. In highly unstable waves, the transverse waves have a range of reactivity, that is rates of reaction in the flow immediately behind the wave. In this study, we present examples of transverse waves for near-limit detonations and analyse four cases in detail. In some cases, these waves appear to be essentially non-reactive or cause very slow reaction. In other cases, the transverse waves can be highly reactive. In the most extreme example, the transverse wave is propagating at the Chapman–Jouguet speed with a small reaction zone, i.e. a transverse detonation. A reactive oblique shock model is used to approximate the triple-point configuration of this case as a double-Mach reflection, which shows good agreement with the images. The reaction evolution along path lines is analysed using detailed reaction mechanisms and considerations about flow-field unsteadiness. Length scales of the energy release and expansion processes within the reaction zone region are used to explain the observed modes of wave propagation and interaction.
Copyright and License
© The Author(s), 2025. Published by Cambridge University Press. This is an Open Access article, distributed under the terms of the Creative Commons Attribution-NonCommercial-NoDerivatives licence (https://creativecommons.org/licenses/by-nc-nd/4.0/), which permits non-commercial re-use, distribution, and reproduction in any medium, provided that no alterations are made and the original article is properly cited. The written permission of Cambridge University Press must be obtained prior to any commercial use and/or adaptation of the article.
Acknowledgement
The authors are grateful to Hadland Imaging for support with the Shimadzu HPV-X2 cameras.
Funding
This work was supported by U.S. Air Force Office of Scientific Research grant FA9550-21-1-0013 (PO: Dr C. Li). M.D.F. acknowledges support from the National Science Foundation Graduate Research Fellowship Program under Grant No. DGE-1333468. One Shimadzu HPV-X2 used in this work was purchased with DURIP grant FA9550-20-1-0226 (PO: Dr C. Li).
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Additional details
- United States Air Force Office of Scientific Research
- FA9550-21-1-0013
- National Science Foundation Graduate Research Fellowship Program
- DGE-1333468
- United States Air Force Office of Scientific Research
- DURIP FA9550-20-1-0226
- Accepted
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2025-06-21
- Available
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2025-08-11Published online
- Caltech groups
- GALCIT, Division of Engineering and Applied Science (EAS)
- Publication Status
- Published