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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2005, Vol. 26 ›› Issue (1): 1-7.

• 论文 •     Next Articles

Two Generations of Unsteady Flow Type for Axial Comperssor

ZHOU Sheng, HOU An-ping, GONG Zhi-qiang, LU Ya-jun, GE Jing-dong   

  1. Department of Jet Prepulsion, Beijing University of Aeronautics and Astronautics, Beijing 10083, China
  • Received:2003-11-25 Revised:2004-03-01 Online:2005-02-25 Published:2005-02-25

Abstract: In order to validate the concept of two generations unsteady flow type-unsteady natural fow type(UNFT)and unsteady cooperative flow type(UCFT)-in axial flow compressor proposed by authors, numerical simulation and experiments are done.It can be seen from the results of numerical simulation that the space-time structure of unsteady flow would translate from chaotic state to orderly state and the time-average performance of flow field can be improved greatly when UCFT is realized.These conclusions also have been validated by our experiments of acoustical excitation and PIV measurement.

Key words: flow type, unsteady separate flow, unsteady natural flow type(UNFT), unsteady cooperative flow type(UCFT), axial flow compressor

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