The averaged velocities and Reynolds stresses were measured at different streamwise positions of a rotating smooth channel with two-dimensional hotwire. The results revealed that: the relatively high local rotation parameter expanded the influence region of rotation on the averaged velocity and induced the relaminarization of the turbulent flow near the leading side. The normalized averaged velocity profiles near the trailing side were strictly arranged in the rotation number order
and presented a logarithmic distribution in the log-law region. Meanwhile
all normalized Reynolds stress components were immune to rotation near the trailing side. Owing to the relaminarization
the normalized averaged velocity profiles near the leading side cannot maintain the logarithmic distribution in the log-law region
and all Reynolds stress components decayed with the growing rotation number and radius of the streamwise position. With the u-v quadrant analysis
the immediate reason of the relaminarization was attributed to the reduction of the generation of turbulent fluctuation.
Experiment of turbulent flow in rotating ribbed channel with TR-PIV
Hot wire test on the flow fields in a rotating square channel
Experiment on characteristics of velocity and temperature fields of rotating boundary layer
Experiment on turbulent flow in rotating smooth channel with 1D hot wire
Mixing characteristics of supersonic mixing layer induced by forced vibration
Related Author
XIA Shuangzhi
LI Haiwang
YOU Ruquan
HU Songjun
SHI Jincheng
LI Hai-wang
DENG Hong-wu
TAO Zhi
Related Institution
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics Astronautics
Collaborative Innovation Center for Advanced Aero-Engine
北京航空航天大学 能源与动力工程学院
北京航空航天大学 前沿科学技术创新研究院
Science and Technology on Scramjet Laboratory, College of Aerospace Science and Engineering, National University of Defense Technology