Experimental study of secondary vortex structures in a rotor wake

2019 ◽  
Vol 60 (11) ◽  
Author(s):  
C. Christian Wolf ◽  
Clemens Schwarz ◽  
Kurt Kaufmann ◽  
Anthony D. Gardner ◽  
Dirk Michaelis ◽  
...  
1988 ◽  
Author(s):  
Chen Fang ◽  
Chen Mao-Zhang ◽  
Jiang Hao-Kang

An experimental study on the production and development of streamwise vortices in a compressor cascade is reported. At four locations inside and one location outside the blade passage, the mean velocity components, three turbulent intensities and three Reynolds stresses were measured with a “x” hot wire probe. The results obtained describe the flow structure in the corner between the end-wall and blade suction surface in detail. Besides a passage vortex within the passage, there exist a shed corner vortex pair and a secondary vortex pair in the corner. The characteristics of two vortex pairs were different from that of the passage vortex. The mechanism causing the shed corner vortex pair and secondary vortex pair and the effect of these vortices on the cascade losses are discussed.


Author(s):  
Ge´rald Kergourlay ◽  
Smai¨ne Kouidri ◽  
Gary W. Rankin ◽  
Robert Rey

This experimental study, applied to a three different sweep axial fan (backward, radial and forward), aims at determining the 3D structure of the rotor wake from unsteady velocity measurements. The hot-film anemometry is used to measure the 3D unsteady velocity components in nearfield, downstream the fan. The data analysis leading to averaged and turbulent velocities, the components of the Reynolds’ stress tensor and the turbulent kinetic energy is presented, in order to illustrate the influence of the sweep. A spectral analysis is also performed.


2011 ◽  
Vol 51 (2) ◽  
pp. 347-359 ◽  
Author(s):  
Hui Hu ◽  
Lucas Clemons ◽  
Hirofumi Igarashi

1992 ◽  
Vol 37 (4) ◽  
pp. 48-57 ◽  
Author(s):  
A. Bagai ◽  
J. G. Leishman

2006 ◽  
Vol 9 (5) ◽  
pp. 413-417 ◽  
Author(s):  
K. Abe ◽  
H. Kihara ◽  
A. Sakurai ◽  
E. Wada ◽  
K. Sato ◽  
...  

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