Abstract
Numerical investigations of high-speed rarefied gas outflow into a vacuum through channels with a forward- or backward-facing step have been conducted using the direct simulation Monte Carlo method. Calculations have been performed for various free-stream Mach numbers, covering transonic, supersonic, and hypersonic flow regimes, and over a wide range of gas rarefaction from free molecular to near hydrodynamic conditions. Mass flow rates through the channel and the gas flow field have been accurately calculated both inside the channel and in the regions upstream and downstream. It has been established that channel geometry, the free-stream velocity, and gas rarefaction strongly influence the gas flow. In the flow field, in front of the channel, a phenomenon known as a detached shock occurs, while inside the channel, a gas recirculation zone may form.
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The datasets generated and analysed during the current study are available from the corresponding author on reasonable request.
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Acknowledgements
This research was supported by the Russian Science Foundation and Government of Sverdlovsk region, Joint Grant No 22-21-20121, https://rscf.ru/en/project/22-21-20121/.
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O.S. wrote the main manuscript text and A.S. prepared figures. All authors reviewed the manuscript.
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Sazhin, O., Sazhin, A. Transonic, supersonic, and hypersonic flow of rarefied gas into vacuum through channels with a forward- or backward-facing step. Microfluid Nanofluid 28, 32 (2024). https://doi.org/10.1007/s10404-024-02727-x
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DOI: https://doi.org/10.1007/s10404-024-02727-x