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Modified AUSMPW+ Scheme and its Application

机译:修改后的AUSMPW +方案及其应用

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摘要

Presented is an investigation into Advection Upstream Splitting Method (AUSM) family schemes.A newly improved version of the AUSM scheme,called AUSMPW+,was developed to increase the accuracy and computational efficiency of AUSM scheme in capturing oblique shock without compromising robustness.With a new definition of the numerical speed of sound at a cell interface,the ability of capturing an oblique shock is remarkably enhanced.Pressure wiggles near wall and shock overshoots across a strong shock are cured by introducing weighting function f based on pressure.In present research,f function was slightly modified to increase the computational efficiency.Extensive numerical test validate that AUSMPW+ scheme with modified function f provide accurate solution of not only transonic but also supersonic flow.The test cases include: (1) SOD shock tube;(2) RAE 2822 airfoil transonic flow; (3) supersonic missile with highly separated flow;(4) AGARD CT5 unsteady test.
机译:本文介绍了对流上游分裂方法(AUSM)系列方案的研究。开发了一种新的改进版AUSM方案AUSMPW +,以提高AUSM方案在不影响稳健性的情况下捕获倾斜冲击的准确性和计算效率。通过在单元界面上定义声音的数值速度,可以显着增强斜向冲击的捕获能力。通过引入基于压力的加权函数f,可以解决壁附近的压力摆动和强烈冲击中的冲击过冲问题。对功能进行了稍许修改以提高计算效率。大量的数值测试证明,修改后的功能f的AUSMPW +方案不仅可以提供跨音速流而且还可以为超音速流提供精确的解决方案。测试案例包括:(1)SOD激波管;(2)RAE 2822翼型跨音速流; (3)高度分离的超音速导弹;(4)AGARD CT5不稳定试验。

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