Existence and uniqueness of axially symmetric compressible subsonic jet impinging on an infinite wall

Jianfeng Cheng, Lili Du, Qin Zhang
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引用次数: 4

Abstract

This paper is concerned with the well-posedness theory of the impact of a subsonic axially symmetric jet emerging from a semi-infinitely long nozzle, onto a rigid wall. The fluid motion is described by the steady isentropic Euler system. We showed that there exists a critical value $M_{cr}>0$, if the given mass flux is less than $M_{cr}$, there exists a unique smooth subsonic axially symmetric jet issuing from the given semi-infinitely long nozzle and hitting a given uneven wall. The surface of the axially symmetric impinging jet is a free boundary, which detaches from the edge of the nozzle smoothly. It is showed that a unique suitable choice of the pressure difference between the chamber and the atmosphere guarantees the continuous fit condition of the free boundary. Moreover, the asymptotic behaviors and the decay properties of the impinging jet and the free surface in downstream were also obtained. The main results in this paper solved the open problem on the well-posedness of the compressible axially symmetric impinging jet, which has proposed by A. Friedman in Chapter 16 in [FA2]. The key ingredient of our proof is based on the variational method to the quasilinear elliptic equation with the Bernoulli's type free boundaries.
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轴对称可压缩亚音速射流撞击无限大壁面的存在唯一性
本文研究了亚音速轴对称射流从半无限长喷嘴向刚性壁面冲击的适定性理论。流体运动用定常等熵欧拉系统描述。我们证明了存在一个临界值$M_{cr}>0$,当给定的质量通量小于$M_{cr}$时,存在一个唯一的光滑亚音速轴对称射流从给定的半无限长喷管射出并击中给定的不均匀壁面。轴对称碰撞射流表面为自由边界,与喷嘴边缘平滑分离。结果表明,对腔室与大气压差的独特选择保证了自由边界的连续拟合条件。此外,还得到了冲击射流和下游自由表面的渐近行为和衰减特性。本文的主要结果解决了A. Friedman在[FA2]第16章中提出的可压缩轴对称冲击射流适定性的开放问题。用变分方法对具有伯努利自由边界的拟线性椭圆型方程进行了证明。
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