首页> 外文会议>Proceedings of the 1st International Symposium on Jet Propulsion and Power Engineering >COMPACT FINITE DIFFERENCE SCHEMES WITH HIGH ORDER OF ACCURACY FOR CAPTURING DISCONTINUITY
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COMPACT FINITE DIFFERENCE SCHEMES WITH HIGH ORDER OF ACCURACY FOR CAPTURING DISCONTINUITY

机译:高精确度的紧致有限差分格式,以捕获不连续性

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In order to suppress numerical oscillations of linear compact schemes around discontinuities, a characteristic-based flux splitting limited method is introduced instead of ENO/WENO or other shock-capturing algorithms. This method begins with upwind schemes and Lax-Friedrich type fluxvector splitting, and variables (fluxes or conservative variables,etc.) are projected along characteristic directions in a difference form, and their amplitudes are carefully controlled by a special limiter in order to meeting entropy criterions and to preventing non-physical oscillations. A fifth-order linear compact upwind scheme is modified by this method for solving problems involving discontinuities. The properties of the numerical algorithm are checked on several classical one-dimensional and multidimensional test cases. Numerical results show it is highorder accurate with high resolution and oscillation-free.
机译:为了抑制不连续附近的线性紧致格式的数值振荡,引入了基于特征的通量分裂限制方法来代替ENO / WENO或其他震荡捕获算法。该方法从迎风方案和Lax-Friedrich型磁通矢量分裂开始,然后沿特征方向以差异形式投影变量(磁通量或保守变量等),并通过特殊的限制器仔细控制其幅度,以满足熵的要求。准则和防止非物理振荡。通过该方法修改了五阶线性紧凑迎风方案,以解决涉及不连续性的问题。在几个经典的一维和多维测试用例上检查了数值算法的属性。数值结果表明,该算法精度高,分辨率高,无振荡。

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