D. Gurak, Mehmet S. Kavsaoglu and I. S. Akmandor, “Multi Block Unsteady Navier Stokes Solution of Com-pressor Stator in Rotor Wake,” 43rd American Institute of Aeronautics and Astronautics (AIAA) aerospace sciences meeting and exhibit, Reno, Nevada, 10-13 January 2005， p. 1011.

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.