首页> 外文会议>Proceedings of the 7th European symposium on aerothermodynamics. >AN EFFECTIVE TREATMENT OF NUMERICAL SHOCKWAVE INSTABILITIES WITH RESIDUAL DISTRIBUTION SCHEMES: APPLICATION TO HYPERSONIC FLOWS AROUND BLUNT BODIES.
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AN EFFECTIVE TREATMENT OF NUMERICAL SHOCKWAVE INSTABILITIES WITH RESIDUAL DISTRIBUTION SCHEMES: APPLICATION TO HYPERSONIC FLOWS AROUND BLUNT BODIES.

机译:具有残余分布方案的数值波波不稳定性的有效处理:应用于钝体周围的超音速流动。

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In the present contribution the issue of simulating hypersonic flows by means of Residual Distribution Schemesrnis discussed. In particular, this discretization techniquernis briefly presented and its current capabilities reviewed.rnCertain aspects of the technique needing some adjustmentsrnto deal with the distinctive characteristics of thernhypersonic regime are identified. Among them, extensivernattention is given to the subject of the carbuncle phenomenon, a critical numerical instability preventing thernaccurate simulation of hypersonic flows around bluntedrnconfigurations. After reviewing the known remedies forrnthis instability, the single one known to be usable in thernResidual Distribution context is presented and studied inrndepth. A sensitivity analysis with respect to its singlerncontrolling parameter is performed. The fix effectivity inrnavoiding the carbuncle is proven. A simple technique torncure an, as far as we know, previously unreported lack ofrnconvergence is presented. The importance of a consistentrntreatment of energy dissipation is assessed, and as a result a complete family of carbuncle fixes is derived. Finally, the numerical treatment is validated for the flow around a cylinder in hypersonic conditions.
机译:在本论文中,讨论了通过剩余分布方案模拟高超音速流动的问题。特别是,简要介绍了这种离散化技术,并回顾了其目前的功能。确定了该技术的某些方面,需要进行一些调整以应对人身制度的独特特征。其中,对carb现象的研究给予了广泛关注,现象是一个关键的数值不稳定性,阻止了围绕钝化构造的高超音速流的准确模拟。在回顾了针对这种不稳定性的已知补救措施之后,提出并深入研究了在残差分布上下文中已知可用的单个补救措施。对其灵敏度控制参数进行灵敏度分析。证明了避免的固定效果。据我们所知,提出了一种简单的技术来解决以前未报告的缺乏收敛性的问题。评估了一致的能量耗散处理的重要性,并因此得出了完整的锁系列。最后,对高超声速条件下圆柱体周围流动的数值处理进行了验证。

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