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No-slip wall acoustic boundary condition treatment in the incompressible limit

机译:不可压缩极限内的防滑墙声边界条件处理

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A characteristic formulation for the numerical treatment of acoustically reflecting no-slip wall boundary condition is presented and numerically validated for some discriminating situations. As an extension of the 3DNSCBC popular approach, this NSWIL strategy relaxes smoothly towards a 3DNSCBC strategy for a slipping wall - the Euler equations natural wall boundary condition - when the viscosity goes to zero. Using our in-house 6th order FD solver, some comparative tests were performed. In particular, we computed a pressure wave train in a 2D periodic channel, leading to standing acoustic waves. Long time runs using NSWIL strategy and involving 2.5 × 10~5 temporal iterations and 2 × 10~3 acoustic reflections at the walls show no numerical instability while popular NSCBC strategy turns out to be unstable after less than 100 reflections. In that case, global mass conservation was very precisely ensured using NSWIL (relative loss <6 × 10~(-5) after 2000 acoustic reflections) while NSCBC induced a global variation above 1% before code crashed.
机译:提出了用于声学反射防滑壁边界条件数值处理的特征公式,并在某些区别情况下进行了数值验证。作为3DNSCBC流行方法的扩展,当黏度为零时,此NSWIL策略可以平滑地向滑墙的3DNSCBC策略(欧拉方程的自然墙边界条件)放松。使用我们内部的六阶FD求解器,进行了一些对比测试。特别是,我们在2D周期性通道中计算了压力波序列,从而产生了驻波。使用NSWIL策略进行长时间运行并涉及2.5×10〜5个时间迭代,并且壁上的2×10〜3个声反射没有数值不稳定,而流行的NSCBC策略在反射少于100次后变得不稳定。在这种情况下,使用NSWIL非常精确地确保了全局质量守恒(2000次声反射后相对损耗<6×10〜(-5)),而NSCBC在代码崩溃之前引起了大于1%的全局变化。

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