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Robust Implementation of High-Order Flux Approximation Schemes for Transonic Flows

机译:跨音速流高阶通量近似方案的稳健实现

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The implementation of high-order rux approximation schemes in thernEZAir suite of structured CFD row solvers is discussed in the currentrnwork. This paper describes the weighted, essentially non-oscillatoryrn(WENO) and monotonicity-preserving (MP) methods that are employedrnfor obtaining up to 5th order of spatial accuracy. The numerical schemes,rnthe test cases, and the results of row simulations conducted to assessrnthe performance of the schemes are detailed. Special focus is given tornthe effects of varying smoothness indicators and other parameters ap-rnpearing in the high-order schemes on the convergence properties, andrnthe demonstrated accuracy of the row solver for subsonic and transonicrnrows. The results highlight the pivotal role of the ϵ parameter in obtain-rning a robust implementation that is suitable for a wide range of rows.
机译:当前工作中讨论了结构化CFD行求解器的EZAir套件中高阶rux逼近方案的实现。本文介绍了加权的,基本上非振荡的(WENO)和保持单调性(MP)的方法,这些方法用于获得高达5阶的空间精度。详细介绍了用于评估方案性能的数值方案,测试案例以及行模拟结果。特别关注了在高阶方案中变化的平滑度指标和其他参数对收敛特性的影响,以及对亚音速和跨音速行的行求解器的准确性进行了证明。结果强调了ϵ参数在获取适用于各种行的可靠实现中的关键作用。

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