Abstract
The turbulent fluctuation and the rotation correction of wall function law are investigated in the entrance section of a rotating channel. The one-dimensional hot wire probe and the X-type probe are utilized to measure the boundary layer at four streamwise stations. Through the analysis on the boundary layer near the leading side and trailing side, it is found that the turbulent fluctuation is promoted in the trailing side whereas suppressed in the leading side. This difference is attributed to the Coriolis instability near the trailing side. In addition, considering the local rotation parameter Rc, whose maximum absolute value is 0.014, is larger than that in previous research, whose maximum value is 0.007, the whole process of the relaminarization is captured. To understand this phenomenon better, the effects of the generation term and the Coriolis term in the transport equation of the Reynolds stress are discussed. In addition, the rotation correction of the viscous-Coriolis region and the Coriolis region are discussed, a new revising method for the wall function is proposed.
| Original language | English |
|---|---|
| Pages (from-to) | 1985-1999 |
| Number of pages | 15 |
| Journal | Chinese Journal of Aeronautics |
| Volume | 31 |
| Issue number | 10 |
| DOIs | |
| State | Published - Oct 2018 |
Keywords
- Coriolis force
- Entry section
- Relaminarization
- Rotating channel
- Turbulence
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