Abstract
The effect of the degree of flow turbulence on detonation processes is analyzed. The relation between the turbulence parameters in front of and behind the shock wave is obtained for the first time. A modified detonation Hugoniot equation is derived, which takes into account the thermal effect and the level of flow turbulence. The equation for determining the velocity of detonation products, which shows how the degree of flow turbulence affects this velocity, was obtained. It is shown that the thermal effect weakens the effect of turbulence. The equation for estimating the effect of heat release and turbulence on the velocity in front of the shock wave is determined.
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The research contribution of authors was funded in frames of the program of research projects of the National Academy of Sciences of Ukraine (No. 6541230) “Support of priority for the state scientific researches and scientific and technical (experimental) developments” 2023–2025 (1230). Project: “Development of technical principles for new high-efficient combustion technology of artificial fuels from solid household waste and biomass in cogeneration energy plants using hydrogen, oxygen, synthetic and biomethane to ensure energy safety.”
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National Academy of Sciences of Ukraine (No. 6541230).
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All authors contributed to the study conception and design. Material preparation, data collection and analysis were performed by A.A. Avramenko, M.M. Kovetskaya, Yu.Yu. Kovetska, A.I. Tyrinov. The first draft of the manuscript was written by Yu.Yu. Kovetska and all authors commented on previous versions of the manuscript. All authors read and approved the final manuscript.
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Avramenko, A., Kovetskaya, M., Kovetska, Y. et al. Normal Detonation Shock Wave in Turbulent Flow. Flow Turbulence Combust (2024). https://doi.org/10.1007/s10494-024-00552-4
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DOI: https://doi.org/10.1007/s10494-024-00552-4