Effect of Multi-rough Element Combination on Hypersonic Boundary Layer

Zhiyi Zhao, Dalei Zhu, Yaodong Yang, Xiaojun Tang, Liang Xin, Guobao Dai, Ao Li
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Abstract

In this paper, the influence of multi-rough element combination controlled by cubic polynomial on the flow field of hypersonic blunt wedge is studied by direct numerical simulation. The influence mechanism of six continuous rough element combinations on the flow parameters in the boundary layer is analyzed in depth, and compared with the influence of double rough elements. It is concluded that the first rough element of the continuous rough element combination has a great influence on the flow field pressure, and the influence of the latter rough element decreases in turn. The combination of six continuous rough elements on the wall can better suppress the incoming flow heating and reduce the wall friction compared with the double rough elements. Compared with smooth wall, wall friction and incoming flow heating are reduced by 25.23 % and 2.69 %, respectively.
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多槽元素组合对高超声速边界层的影响
本文通过直接数值模拟研究了由三次多项式控制的多粗糙元素组合对高超声速钝楔流场的影响。深入分析了六种连续粗糙元素组合对边界层流动参数的影响机理,并与双粗糙元素的影响进行了比较。结论是连续粗糙元素组合中第一个粗糙元素对流场压力的影响较大,后一个粗糙元素的影响依次减小。与双粗糙元件相比,壁面上的六个连续粗糙元件组合能更好地抑制来流加热,减少壁面摩擦。与光滑壁面相比,壁面摩擦和入流加热分别减少了 25.23 % 和 2.69 %。
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