Shaobin Li, Fu Chen and Peigang Yan, “Numerical In-vestigation of the Effect of Stator Clocking on Blade Boundary Layer Flow in Compressor,” Acta Aeronautica Et Astronautica Sinica, Vol. 28, No. z1, 2007, pp. s62-69.

has been cited by the following article:

• TITLE: Investigation of Stator Wake Variability in Single Stage Axial-Compressor

  AUTHORS: Xiaorong Xiang, Bo Liu, Liqing Qiao, Qingwei Wang

  KEYWORDS: Axial-Flow, Compressor, Wake, Hot-Wire Anemometer (HWA), Vorticity

  JOURNAL NAME: Engineering, Vol.2 No.7, July 23, 2010

  ABSTRACT: In this paper, we investigate the stator wake variability along the axial direction under different rotating speeds and mass flow conditions, in the terms of wake-core position, wake depth, wake width and wake velocity gradient. Experimental study is carried out in a single stage axial compressor by using Hot-wire Anemometer (HWA). Simultaneously, the numerical calculation is brought out in the same experiment rig. Firstly, we analyze the time-averaged velocity and radial vorticity at different axial positions, and explore the wake variability along the axial direction. Then, we present the effects of operation conditions on the wake-core position, and find out the inlet Mach number and incident angle are both the key influence factors of the wake-core position. Finally, we summarize four preliminary conclusions of the wake variability.