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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1994, Vol. 15 ›› Issue (4): 472-475.

• 论文 • Previous Articles     Next Articles

EXPERIMENT INVESTIGATION FOR THE INNER-RING PROFILE ANDITS ROTATING EFFECT OF A NEW TYPE OF AXIAL FLOW VANELESS NOZZLE

Liu Jingmei1, Liu Bin2, Xiang Yimin2   

  1. 1. Department of Jet Propulsion,Beijing University of Aeronautics and Astronautics,Beijng,100083;2. Xi'an Jiaotong University, Xi'an,710049
  • Received:1992-05-03 Revised:1993-06-07 Online:1994-04-25 Published:1994-04-25

Abstract: n this paper,a test rig is set up for experiment investigation to axial double flow vaneless nozzle and three different profiles of inner-ring are designed for it.Pentahole probes and nicro-trihole bOundary layer probes are employed for measuring the radial parameters dis-tribution. The flow field of this new type of nozzle is analysed and the optimum profile of inner-ring and velocity coefficient are obtained.Additionally,the rotating effect of the inner-ring can keep the losses lower.This new type of nozzle can be applied in the large power turbines as the first stage.

Key words: axial flow vaneless nozzle, inner-ring profile, experimental data

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