来自AIAA的论文
《Supersonic laminar flow control on swept wings using distributed roughness》
中间提到一个叫做:
The distortion results in saturation of the primary
wave and growth of harmonics. Saturation appears well
before transition. The saturation amplitude appears to be independent of the leading-edge roughness amplitude.
以上这些该怎么理解呢?
谢谢