PIV Measurement and CFD Analysis for the Shear Flows between Static and Rotating Disks

2002 ◽  
Vol 2002.77 (0) ◽  
pp. _13-47_-_13-48_
Author(s):  
Shigeru MURATA ◽  
Shuichi KIZAWA
Author(s):  
Masamichi Koyama ◽  
Hiroshi Fujiwara ◽  
Laurent Zimmer ◽  
Shigeru Tachibana

In this paper, flow fields inside a premixed combustor have been investigated by CFD analysis and PIV measurement in a preheating, non-reacting condition. Four types of premixer are examined. The design of the premixer is determined by the combination of swirlers and mixing tubes. There are two variations of triple-concentric swirlers and three variations of mixing tubes. Comparisons are made among mean velocity distributions derived from CFD and PIV. PDF analysis is performed on the data from PIV to discuss the possibility of the occurrence of flashback. Combustion rig tests have been carried out also on similar condition to see combustion instabilities depending on the choice of premixers and operating conditions. Flame is directly observed from crystal windows placed on the side and downstream of the combustion chamber. A glass rod is installed on the wall of the mixing tube so as to see light emissions inside the tube, i.e. evidence of flashback. Pressure fluctuations at the combustor liner are measured in one position. The spectra of pressure fluctuations are computed to look at the possibility of combustion oscillations. Discussions are made on the relation between the global flame structure and pressure modes. Finally, proper premixer configurations to prevent combustion instabilities are proposed.


2004 ◽  
Vol 2004.53 (0) ◽  
pp. 277-278
Author(s):  
Shigeyuki Tomimatsu ◽  
Yayoi Yonayama ◽  
Kazuo Uranishi

2017 ◽  
Vol 16 (3) ◽  
pp. 163-173 ◽  
Author(s):  
Akiko Sugahara ◽  
Hisahi Kotani ◽  
Yoshihisa Momoi ◽  
Toshio Yamanaka ◽  
Kazunobu Sagara ◽  
...  

2017 ◽  
Vol 2017.92 (0) ◽  
pp. M703
Author(s):  
Shouhei Tsugawa ◽  
Ryosuke Uenishi ◽  
Morihiko Uesaka ◽  
Takashi Watanabe ◽  
Hirochika Tanigawa ◽  
...  

2004 ◽  
Vol 24 (Supplement1) ◽  
pp. 149-152
Author(s):  
Koichi NISHINO ◽  
Daisuke KAWAGUCHI ◽  
Hidetaka SATO ◽  
Haruo ISODA ◽  
Takashi KOSUGI

Author(s):  
Yukie Sasaki ◽  
Koutarou Hisaeda ◽  
Shinsuke Matsuno ◽  
Takahisa Nagao ◽  
Junya Kouwa

In this paper, in order to improve temperature prediction, 2D axisymmetric CFD analysis has been implemented to determine the cavity flow network in Finite Difference Method (FDM) thermal analysis model. With this work process, for example, the complex recirculation of cavity flow can be considered in FDM thermal analysis. In the beginning, the rig test of simplified cavity with rotating disk and PIV measurement are carried out to investigate the flow structure in the cavity and to validate CFD analysis. CFD result has matched well with the measurement data of PIV, and it has been found that SST k-ω turbulent model provides the most reliable result by the sensitivity study. The study result also helps to choose the most suitable scheme of discretization and the method of pressure correction. Then, the modeling of the cavity flow network based on CFD analysis result has been applied to the thermal analysis for the aero-engine. Compared with the measured data, the result with this modeling shows that temperature prediction has been well improved.


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