Experimental study of hypersonic boundary layer transition on a flat plate delta wing
Experimental Thermal and Fluid Science(2020)
摘要
•The behavior of boundary layer transition on a delta wing was studied.•Boundary layer transition on side line is earlier than that on center line.•Low frequency large scale structures induce to boundary layer transition.•Nonlinear interaction prior to transition is stronger than turbulent boundary layer.•Unstable region of disturbance waves depends on the Reynolds number.
更多查看译文
关键词
Delta wing,Hypersonic boundary layer,Transition,Second mode waves
AI 理解论文
溯源树
样例
![](https://originalfileserver.aminer.cn/sys/aminer/pubs/mrt_preview.jpeg)
生成溯源树,研究论文发展脉络
Chat Paper
正在生成论文摘要