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STABILITY OF TRANSONIC JETS WITH STRONG RAREFACTION WAVES FOR TWO-DIMENSIONAL STEADY COMPRESSIBLE EULER SYSTEM

机译:二维稳态可压缩EULER系统中具有强反射波的跨音速飞机的稳定性

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We study supersonic flow past a convex corner which is surrounded by quiescent gas. When the pressure of the upstream supersonic flow is larger than that of the quiescent gas, there appears a strong rarefaction wave to rarefy the supersonic gas. Meanwhile, a transonic characteristic discontinuity appears to separate the supersonic flow behind the rarefaction wave from the static gas. In this paper, we employ a wave front tracking method to establish structural stability of such a flow pattern under non-smooth perturbations of the upcoming supersonic flow. It is an initial-value/free-boundary problem for the two-dimensional steady non-isentropic compressible Euler system. The main ingredients are careful analysis of wave interactions and construction of suitable Glimm functional, to overcome the difficulty that the strong rarefaction wave has a large total variation.
机译:我们研究经过一个被静态气体包围的凸角的超音速流动。当上游超音速流的压力大于静态气体的压力时,会出现强烈的稀疏波以使超音速气体稀化。同时,跨音速特征的不连续性似乎将稀疏波后面的超音速流与静态气体分开。在本文中,我们采用波前跟踪方法来建立这种流动模式在即将到来的超音速流动的非光滑扰动下的结构稳定性。对于二维稳态非等熵可压缩欧拉系统,这是一个初值/自由边界问题。主要成分是仔细分析波相互作用和构建合适的Glimm官能团,以克服强稀疏波具有较大的总变化的困难。

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