Abstract
In this paper, a singularly perturbed problem for the stable fluid flow is considered. As supersonic speed at upper reaches and subsonic speed at lower reaches in a duct, the position of shock layer is analyzed and the asymptotic estimation of solution, is obtained.
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References
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Jiaqi, M. A singularly perturbed problem for stable supersonic flow. Appl. Math. Chin. Univ. 14, 153–157 (1999). https://doi.org/10.1007/s11766-999-0021-2
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DOI: https://doi.org/10.1007/s11766-999-0021-2