Multi-scale geometric analysis of evolving Lagrangian structures in the compressible transitional boundary layer at $Ma=0.7$
ORAL
Abstract
Evolutionary geometry of flow structures in a compressible transitional boundary layer at $Ma=0.7$ is investigated from a Lagrangian perspective. The Lagrangian structures in the transition are extracted from the Lagrangian scalar field by a moving window filter, and then their geometry is characterized by the multi-scale and multi-directional geometric analysis (Yang and Pullin, \emph{J. Fluid Mech.}, 674, 2011), including the averaged inclination and sweep angles at different scales ranging from one half of the boundary layer thickness to several viscous length scales $\delta_\nu$. The results show that averaged angles are almost unaltered for different scales before the transition. As the transition occurs, averaged inclination angles increase and sweep angles decrease rapidly with increasing reference time. Furthermore, the orientation changes more significantly for structures with small scales than large scales. In the late stage of transition, the averaged inclination angle of small-scale structures with the length scale $\sim O(10)\delta_\nu$ is $42\,^{\circ}$, and the averaged sweep angle in the logarithm law region is approximately $30\,^{\circ}$.
–
Authors
-
Wenjie Zheng
State Key Laboratory for Turbulence and Complex Systems, College of Engineering, Peking University, Beijing 100871, China
-
Yue Yang
Peking University, State Key Laboratory for Turbulence and Complex Systems, College of Engineering, Peking University, Beijing 100871, China, State Key Laboratory for Turbulence and Complex Systems, College of Engineering, Peking University
-
Shiyi Chen
State Key Laboratory for Turbulence and Complex Systems, College of Engineering, Peking University, Beijing 100871, China