Numerical Analysis of Nozzle Clearance's Effect on Turbine Performance

2011 ◽  
Vol 24 (04) ◽  
pp. 618 ◽  
Author(s):  
Liangjun HU
Author(s):  
Eunhwan Jeong ◽  
Pyun Goo Park ◽  
Sang Hun Kang ◽  
Jinhan Kim

This paper presents the results of performance test and numerical analysis of a supersonic impulse turbine. The test has been conducted using high pressure cold air. The overall turbine performance and turbine nozzle behavior for various operating conditions have been investigated. Experiment and numerical analysis also have been conducted to investigate the nozzle-rotor clearance effect on the turbine performance. It has been found that turbine performance degrades with increasing the axial clearance and this phenomenon is mainly due to the increased stagnation pressure loss in the axial clearance region.


2019 ◽  
Vol 158 ◽  
pp. 1986-1992 ◽  
Author(s):  
Dongdong Liu ◽  
Yanyan Chen ◽  
Wei Dai ◽  
Ercang Luo

Energy ◽  
2018 ◽  
Vol 159 ◽  
pp. 827-841 ◽  
Author(s):  
Aki Grönman ◽  
Jari Backman ◽  
Markus Hansen-Haug ◽  
Mikko Laaksonen ◽  
Markku Alkki ◽  
...  

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