TY - GEN
T1 - Critical Regions Driving Unsteady Wake Dynamics in Flow Past Multi-Cylinder Arrays
AU - Thazhathattil, Vivek
AU - Hemchandra, Santosh
AU - Mohanty, Pratikshya
AU - Islam, Syed Tawsif
AU - O’connor, Jacqueline
N1 - Publisher Copyright:
© 2026, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2026
Y1 - 2026
N2 - Large-eddy simulation (LES) is used to determine the time-resolved flow evolution past two cylinders placed side by side. The simulations are conducted at a nominal Reynolds number of ReD = 10000. Complex network analysis is applied to the resulting datasets to identify the location and spatial extent of the flow regions that govern the unsteady wake dynamics. A nominal single-cylinder configuration with well-established reference data is employed to benchmark the LES. For the closely spaced two-cylinder case, an asymmetric time-averaged f low structure with a biased inter-cylinder gap flow is observed. This configuration exhibits a broad and a narrow wake, with the former driving the vortex shedding in the near wake. The widely spaced case presents a symmetric time-averaged flow structure, with vortex shedding from both wakes that interact further downstream. Complex networks are constructed for the single-cylinder case using correlation, mutual information, and transfer entropy to quantify nodal connectivity. These networks exhibit prominent hubs when mapped back into physical space, thereby identifying the wave maker region that drives the downstream wake dynamics, consistent with prior studies. For the closely spaced two-cylinder case, the network analysis reveals a wave maker only within the broad-wake region, while a more symmetric wave maker distribution is observed in the widely spaced case.
AB - Large-eddy simulation (LES) is used to determine the time-resolved flow evolution past two cylinders placed side by side. The simulations are conducted at a nominal Reynolds number of ReD = 10000. Complex network analysis is applied to the resulting datasets to identify the location and spatial extent of the flow regions that govern the unsteady wake dynamics. A nominal single-cylinder configuration with well-established reference data is employed to benchmark the LES. For the closely spaced two-cylinder case, an asymmetric time-averaged f low structure with a biased inter-cylinder gap flow is observed. This configuration exhibits a broad and a narrow wake, with the former driving the vortex shedding in the near wake. The widely spaced case presents a symmetric time-averaged flow structure, with vortex shedding from both wakes that interact further downstream. Complex networks are constructed for the single-cylinder case using correlation, mutual information, and transfer entropy to quantify nodal connectivity. These networks exhibit prominent hubs when mapped back into physical space, thereby identifying the wave maker region that drives the downstream wake dynamics, consistent with prior studies. For the closely spaced two-cylinder case, the network analysis reveals a wave maker only within the broad-wake region, while a more symmetric wave maker distribution is observed in the widely spaced case.
UR - https://www.scopus.com/pages/publications/105031078645
UR - https://www.scopus.com/pages/publications/105031078645#tab=citedBy
U2 - 10.2514/6.2026-0947
DO - 10.2514/6.2026-0947
M3 - Conference contribution
AN - SCOPUS:105031078645
SN - 9781624107658
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026
BT - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026
Y2 - 12 January 2026 through 16 January 2026
ER -