主管部门: 中国航天科技集团有限公司
主办单位: 中国航天空气动力技术研究院
中国宇航学会
中国宇航出版有限责任公司

边条周向位置对钝头体非对称流动的影响

Effect of Circumferential Angle of Strake on Asymmetric Flow Over Blunt-Nosed Body

  • 摘要: 在大迎角飞行时,钝头体会产生非对称流动,进而引起不确定的侧向力。在钝头体的头部施加一定高度的边条可以控制这种非对称流动。为了研究边条周向位置对非对称背涡结构的影响,在攻角50°和Reynolds数为1.68×105的条件下,通过数值模拟和风洞实验,对比了不同高度的边条处于不同周向位置时钝头体的流动结构。研究结果表明,当边条绕模型周向旋转一周时,侧向力的扰动响应关系随边条高度的变化而发生变化。边条所产生的流动在模型背风侧的演化直接影响了边条对非对称流动的主控作用,当边条高度较小时,边条位于迎风侧和背风侧对非对称流动的主控作用一致。当边条高度较大时,边条位于迎风和背风侧,其旋涡的演化形式存在差异,对非对称流动的主控作用相反。

     

    Abstract: At a high angle of attack, asymmetric flow will be generated on the blunt-nosed body, leading to unpredictable side force. The regulation of asymmetric flow can be achieved by applying strakes with a specific height to the nose of the blunt-nosed body. To investigate the effect of the circumferential position of the strake on the asymmetric flow of a blunt-nosed body, the flow structures were analyzed at an angle of attack of 50° and a Reynolds number of 1.68×105, where the strake was placed at different heights and circumferential angles. The research findings indicate that the response relationship of the side force varies with the alteration of the strake height as the strake rotates circumferentially around the nose. The flow generated by the strake has a direct impact on the dominant role of the strake in controlling the asymmetric flow through the evolution on the leeward side of the model. When the height of strake is small, the control effect on the asymmetric flow is consistent irrespective of whether the strake is situated on the windward or leeward side. When the height is large, the evolution pattern of the vortex generated by the strake varies depending on whether the strake is located on the windward or leeward side, and the control effect on the asymmetric flow is opposite.

     

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