波纹壁面上的高超声速边界层气动降热（英文）

作者：朱文凯; 顾丁炜; 司武飞; 陈十一; 朱一丁^*; 李存标^*

来源：Science Bulletin, 2022, 67(10): 988-990.

<正>Hypersonic boundary layer transition is of fundamental importance for the design of high-speed vehicles because of its direct relevance to drag and aerodynamic heating. As the focus of transition and turbulence research is shifting towards higher velocities,research on compressible flows, especially hypersonic flows, is becoming increasingly attractive to researchers worldwide [1,2].

• 单位
  湍流与复杂系统国家重点实验室; 北京大学