TY - GEN
T1 - The effect of crossflow on vortex rings
AU - Sau, Rajes
AU - Mahesh, Krishnan
PY - 2007
Y1 - 2007
N2 - DNS is performed to study passive scalar mixing in vortex rings in the presence, and absence of crossflow. For vortex rings without crossflow, the 'formation number' (Gharib et. al 1998) is found to be 3.6. Simulations are performed for a range of stroke ratios encompassing the formation number. In the absence of crossflow, the optimal stroke ratio for mixing and entrainment is shown to be at the formation number; the trailing column is not seen to be as beneficial as the ring itself. However, in the presence of crossflow, the trailing column is shown to contribute significantly to the overall mixing and entrainment. The trailing column enhances the entrainment significantly because of the high pressure gradient created by deformation of the column upon interacting with crossflow. It is shown that the crossflow reduces the stroke ratio beyond which the trailing column forms. This reduction in stroke ratio is due to entrainment of crossflow fluid during formation of the ring, and depends on the velocity ratio.
AB - DNS is performed to study passive scalar mixing in vortex rings in the presence, and absence of crossflow. For vortex rings without crossflow, the 'formation number' (Gharib et. al 1998) is found to be 3.6. Simulations are performed for a range of stroke ratios encompassing the formation number. In the absence of crossflow, the optimal stroke ratio for mixing and entrainment is shown to be at the formation number; the trailing column is not seen to be as beneficial as the ring itself. However, in the presence of crossflow, the trailing column is shown to contribute significantly to the overall mixing and entrainment. The trailing column enhances the entrainment significantly because of the high pressure gradient created by deformation of the column upon interacting with crossflow. It is shown that the crossflow reduces the stroke ratio beyond which the trailing column forms. This reduction in stroke ratio is due to entrainment of crossflow fluid during formation of the ring, and depends on the velocity ratio.
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U2 - 10.2514/6.2007-1316
DO - 10.2514/6.2007-1316
M3 - Conference contribution
AN - SCOPUS:34250851791
SN - 1563478900
SN - 9781563478901
T3 - Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting
SP - 15673
EP - 15686
BT - Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 45th AIAA Aerospace Sciences Meeting 2007
Y2 - 8 January 2007 through 11 January 2007
ER -