Summary
In this paper, we have postulated, in a conducting gas, the occurrence of a boundary shock wave, considered as a quick transition region in which the viscous effects are compressive and are confined to a thin layer adjacent to a surface. The analogues of the well known Rankine-Hugoniot jump relations, Prandtl relation, and other properties of a shock wave are derived and a discussion about the existence of a boundary shock wave is made.
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References
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Verma, B.G., Prasad, B. Boundary shock waves in a conducting gas. PAGEOPH 87, 203–209 (1971). https://doi.org/10.1007/BF00878924
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DOI: https://doi.org/10.1007/BF00878924