Propagation of a shock wave through a viscous heat-conducting gas in a long microchannel
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Publication:2322140
DOI10.1134/S0015462819020034zbMath1421.76146OpenAlexW2955880344WikidataQ127520854 ScholiaQ127520854MaRDI QIDQ2322140
Publication date: 3 September 2019
Published in: Fluid Dynamics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1134/s0015462819020034
Riemann problemshock waveboundary layerrarefied gasmolecular beamcomplex conservative difference scheme
Shock waves and blast waves in fluid mechanics (76L05) Finite difference methods applied to problems in fluid mechanics (76M20)
Cites Work
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- Complex conservative difference schemes for computing supersonic flows past simple aerodynamic forms
- Unsteady rarefied gas flow with shock wave in a channel
- Unsteady rarefied gas flow in a microchannel driven by a pressure difference
- Solution of the Boltzmann equation for unsteady flows with shock waves in narrow channels
- Shock-Tube Performance at Low Initial Pressure
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