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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1994, Vol. 15 ›› Issue (12): 1512-1514.

• 论文 • Previous Articles     Next Articles

A PRELIMINARY EXPERIMENTAL STUDY ON LOBED NOZZLE EJECTOR SYSTEM

Zhang Jingzhou, LiLiguo, Gao Chao   

  1. Second Department of Nanjing University of Aeronautics and Astronautics, Nanjing, 210016
  • Received:1993-09-17 Revised:1994-04-15 Online:1994-12-25 Published:1994-12-25

Abstract: he lobed nozzle and round nozzle experiments,both with the same exit areas,are in low pressure ratio ejector systems to investigate the pumping capability and mixing efficiency.And the 3-D flow fields inside the lobed nozzle ejector are measured.The results show that the ejector pumping capability and nuxing efficiency are obviously improved by using the lobed noz-zle which can generate large-scale axial vortiees and cause lower static pressure at the nozzle exit.

Key words: ejector, mixing flow, nozzle, lobed nozzle

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