Compressible subsonic jet flows issuing from a nozzle of arbitrary cross-section
Research output: Journal Publications and Reviews (RGC: 21, 22, 62) › 21_Publication in refereed journal › peer-review
Author(s)
Related Research Unit(s)
Detail(s)
Original language | English |
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Pages (from-to) | 5318-5359 |
Journal / Publication | Journal of Differential Equations |
Volume | 266 |
Issue number | 9 |
Online published | 5 Nov 2018 |
Publication status | Published - 15 Apr 2019 |
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Abstract
We are concerned with the well-posedness theory of two-dimensional compressible subsonic jet flow issuing from a semi-infinitely long nozzle of arbitrary cross-section. Given any atmospheric pressure p0, we show that there exists a critical mass flux mcr depending on p0 and Ω such that if the incoming mass flux m0 is less than the critical value, then there exists a unique smooth subsonic jet flow, issuing from the given nozzle. The jet boundary is a free streamline, which initiates from the end point of the nozzle smoothly and extends to the infinity. One of the key observations in this paper is that the restriction of the incoming mass flux guarantees completely the subsonicity of the compressible jet in the whole flow field, which coincides with the observation on the compressible subsonic flows in an infinitely long nozzle without free boundary in [8].
Research Area(s)
- Euler system, Existence, Free boundary, Subsonic jet, Uniqueness
Citation Format(s)
Compressible subsonic jet flows issuing from a nozzle of arbitrary cross-section. / Cheng, Jianfeng; Du, Lili; Xiang, Wei.
In: Journal of Differential Equations, Vol. 266, No. 9, 15.04.2019, p. 5318-5359.Research output: Journal Publications and Reviews (RGC: 21, 22, 62) › 21_Publication in refereed journal › peer-review