0641 Experimental Study on a Separated Flow behind a Backward-Facing Step (Two-Dimensional Measurement by the Flying Hot-Wire Technique)

2013 ◽  
Vol 2013 (0) ◽  
pp. _0641-01_-_0641-02_
Author(s):  
Yoshihiro INOUE ◽  
Hirotoshi SATO ◽  
Naoya SUGIURA
1999 ◽  
Vol 121 (2) ◽  
pp. 441-445 ◽  
Author(s):  
O. O. Badran ◽  
H. H. Bruun

This paper is concerned with measurements of the flow field in the separated flow region behind a backward-facing step. The main instrument used in this research was Flying X Hot-Wire Anemometry (FHWA). Stationary (single normal) Hot-Wire Anemometry (SHWA) was also used. Comparative measurements between the SHW probe and the FHW system were conducted downstream of the step (step height H = 120 mm) and results are presented for axial locations of 1H and 2H. Two step configurations were considered; (i) a blunt leading edge with flow underneath (Case I) and (ii) a blunt leading edge with no flow underneath (Case II). It is observed from the results presented that the two Hot-Wire methods produce significantly different mean velocity and turbulence results inside the separation bubble. In particular, the SHWA method cannot detect the reverse flow velocity direction, while the Flying Hot-Wire clearly identifies the existing reverse flow. Also, in the shear flow region, the results presented indicate that measurements with a SHW probe must be treated with great caution.


Author(s):  
Taisuke Murayama ◽  
Katsuya Hirata ◽  
Jiro Funaki

This research concerns the jet from an asymmetrical two-dimensional nozzle, especially about the influence of the lip length of the nozzle. The authors conduct experiments at a Reynolds number Re of 6000. The aspect ratio of the nozzle exit is fixed to 300. And, the lip length is 0, 2.0h, 3.3h and 5.0h, where h denotes the height of the nozzle exit. Using a hot-wire-anemometer, the authors show mean-velocity profiles at various downstream sections, in order to reveal fundamental characteristics of the jet in both the near and far downstreams. Furthermore, in the near downstream, the authors visualise the flow by smoke so as to get quantitative information using a PIV technique, and perform the dominant-frequency measurements.


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