Control of crossflow vortex in a swept wing boundary layr

虽然后掠翼和旋转盘的流场是相同的，但预测横流不稳定开始条件的风量纲参数是不同的，通过本文的研究，提出了一个可用于一般横流不稳定场的新参数。当该参数值达到10时，可以预测二次失稳的起始条件。结果如参考文献所示。2.还得到了一个重要的结果，即流向横流涡旋一旦出现，它就不会移动，而是停留在原地。它说明了使用本地控制系统逐个控制每个涡旋的可能性。这种控制系统应该在下一步的研究中立即开发出来。

Von-dimensional parameters which predicts the onset condition for crossflow instability have been different ones for a swept wing and a rotating disk although the flow fields are same.Through present investigation, a new parameter which can be used for general crossflow instability field. Onset condition can be predicted when the value of this parameter reaches 10.Onset conditions for the secondary instability is also obtained. Results are shown in Ref. 2.It is also important results that once a streamwise crossflow vortex appear, it will not move, and stays where it is. It tells the possibility that one might control each vortex one by one using local control system. Such control system should be instensively developed in the next research steps.