In this paper, the Vogel–Escudier flow is studied at an aspect ratio of 2.5 and a Reynolds number range of 330–3000. An attempt is made to control the vortex breakdown bubbles using a thin rod in co- and counter-rotation cases. The flow is studied qualitatively using planar laser-induced fluorescence and quantitatively using particle image velocimetry measurements. In terms of swirl strength, defined as the ratio of Reynolds numbers of the disk and control rod, a complete suppression and subsequent reemergence of vortex breakdown bubbles is observed at 56 and 37, respectively. Counter-rotation shows a slight decrease until −150 and a periodic and aperiodic shedding of the vortices at −112 and −75. An attempt is made to explain the flow behavior by experimental and analytical means taking into consideration the azimuthal plane flow using the swirl decay mechanism. Further, experiments are performed for time varying co- and counter-rotations for various combinations of amplitude and frequency. The anomalous behavior at high frequencies of destabilization of vortices in co-rotation and a milder change in counter-rotation is observed.
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September 2021
Research Article|
September 21 2021
Vortex breakdown control using varying near axis swirl
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Shreya Sharma
;
Shreya Sharma
Department of Aerospace Engineering, Indian Institute of Technology-Kanpur
, Kanpur, Uttar Pradesh 208 016, India
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Praneeta B. Sachan
;
Praneeta B. Sachan
Department of Aerospace Engineering, Indian Institute of Technology-Kanpur
, Kanpur, Uttar Pradesh 208 016, India
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Navneet Kumar;
Navneet Kumar
Department of Aerospace Engineering, Indian Institute of Technology-Kanpur
, Kanpur, Uttar Pradesh 208 016, India
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Rahul Ranjan;
Rahul Ranjan
Department of Aerospace Engineering, Indian Institute of Technology-Kanpur
, Kanpur, Uttar Pradesh 208 016, India
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Sanjay Kumar
;
Sanjay Kumar
a)
Department of Aerospace Engineering, Indian Institute of Technology-Kanpur
, Kanpur, Uttar Pradesh 208 016, India
a)Author to whom correspondence should be addressed: [email protected]
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Kamal Poddar
Kamal Poddar
Department of Aerospace Engineering, Indian Institute of Technology-Kanpur
, Kanpur, Uttar Pradesh 208 016, India
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Shreya Sharma
Praneeta B. Sachan
Navneet Kumar
Rahul Ranjan
Sanjay Kumar
a)
Kamal Poddar
Department of Aerospace Engineering, Indian Institute of Technology-Kanpur
, Kanpur, Uttar Pradesh 208 016, India
a)Author to whom correspondence should be addressed: [email protected]
Physics of Fluids 33, 093606 (2021)
Article history
Received:
June 23 2021
Accepted:
August 25 2021
Citation
Shreya Sharma, Praneeta B. Sachan, Navneet Kumar, Rahul Ranjan, Sanjay Kumar, Kamal Poddar; Vortex breakdown control using varying near axis swirl. Physics of Fluids 1 September 2021; 33 (9): 093606. https://doi.org/10.1063/5.0061025
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