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Stability Analysis: an experimental study of stationary crossflow instability for swept wing boundary layer

机译:稳定性分析:机翼后掠边界层固定横流不稳定性的实验研究

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The present work addressed a new stability analysis progress to probe out the optimal wavelength of crossflow (CF) instability for infinity spanwise swept wing. Though the development of nonlinearity is noticed, the new analysis progress shows an efficient way to find out the optimal wavelength via linear method base on the similar work in Arizona State University (ASU). The characteristics of result of Orr-Sommerfel (O-S) equation in the linear region are developed as the new criteria. In the end, according to the optimal wavelength got by our new criteria, discrete micron-sized roughness elements array control experiments are conducted to validate the former conclusion, and transition is delayed distinctly.
机译:本工作解决了一项新的稳定性分析进展,以探究无限翼展后掠机翼的最佳横波(CF)失稳波长。尽管注意到了非线性的发展,但新的分析进展表明,在亚利桑那州立大学(ASU)的类似工作的基础上,可以通过线性方法找到最佳波长的有效方法。线性区域中的Orr-Sommerfel(O-S)方程的结果的特征被开发为新的标准。最后,根据我们的新标准获得的最佳波长,进行了离散微米级粗糙度元件阵列控制实验,以验证先前的结论,并且过渡明显延迟。

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