• Acta Physica Sinica
  • Vol. 69, Issue 13, 134701-1 (2020)
Li-Jun Hu1、*, Hai-Zhuan Yuan2, and Yu-Long Du3
Author Affiliations
  • 1School of Mathematics and Statistics, Hengyang Normal University, Hengyang 421002, China
  • 2School of Mathematics and Computational Science, Xiangtan University, Xiangtan 411105, China
  • 3School of Mathematical Sciences, Beihang University, Beijing 100191, China
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    DOI: 10.7498/aps.69.20191851 Cite this Article
    Li-Jun Hu, Hai-Zhuan Yuan, Yu-Long Du. A modified HLLEM scheme and shock stability analysis[J]. Acta Physica Sinica, 2020, 69(13): 134701-1 Copy Citation Text show less

    Abstract

    Reliable numerical simulations for hypersonic flows require an accurate, robust and efficient numerical scheme. The low-dissipation shock-capturing methods often suffer various forms of shock wave instabilities when used to simulate hypersonic flow problems numerically. For the two-dimensional(2D) inviscid compressible Euler equations, the stability analysis of the low-dissipation HLLEM scheme is conducted. The odd and even perturbations are added to the initial state in the streamwise direction and the transverse direction respectively, and the evolution equations of perturbations are deduced to explore the mechanism of instability inherent in the HLLEM scheme. The results of stability analysis show that the perturbations of density and shear velocity in the flux transverse to the shock wave front are undamped. Due to the symmetry, the 2D Sedov blast wave problem is computed to prove the multidimensionality of the shock instability. In the one-dimensional case which is free from the instability, the undamped property of density perturbation is also existent but no shear velocity is found. The conclusion can be drawn as follows: the shock instability of HLLEM scheme is triggered by the perturbation growth of shear velocity in the flux transverse to the shock wave front. Based on the conclusion of stability analysis, the instability of HLLEM scheme is cured by adding the shear viscosity to the transverse flux. In order to avoid affecting the resolution of the shear layer due to the introduction of too high shear viscosity, two functions to detect the shock wave and the subsonic regimes are defined, so that the shear viscosity is only added to the transverse flux in the subsonic regime of the shock layer, while the rest of numerical fluxes are still computed by the original HLLEM scheme. The results of stability analysis and some challenging numerical test problems show that the modified HLLEM scheme not only retains the merits of the original HLLEM, such as, resolving contact discontinuity and shear wave accurately, but also has greatly improved its robustness, inhibiting the unstable phenomena from occurring effectively when computing the strong shock wave problems.
    Li-Jun Hu, Hai-Zhuan Yuan, Yu-Long Du. A modified HLLEM scheme and shock stability analysis[J]. Acta Physica Sinica, 2020, 69(13): 134701-1
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