导航
ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1994, Vol. 15 ›› Issue (4): 472-475.
• 论文 • Previous Articles Next Articles
Liu Jingmei1, Liu Bin2, Xiang Yimin2
Received:
Revised:
Online:
Published:
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
CLC Number:
TK249.263.4
Liu Jingmei;Liu Bin;Xiang Yimin. EXPERIMENT INVESTIGATION FOR THE INNER-RING PROFILE ANDITS ROTATING EFFECT OF A NEW TYPE OF AXIAL FLOW VANELESS NOZZLE[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1994, 15(4): 472-475.
/ / Recommend
Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks
URL: https://hkxb.buaa.edu.cn/EN/
https://hkxb.buaa.edu.cn/EN/Y1994/V15/I4/472