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May 14, 2026Physics of Fluids0 citations

The role of the remnant vortex in the wake instability of a heaving and pitching foil in quiescent fluid

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GPGangadhar V. R. PinapatruniKKKalyani KalavakuntaSNSarath Nagirikatakam

Key Points

  • This research investigates how a remnant vortex influences wake instability in a heaving and pitching airfoil.
  • Experimental and numerical approaches were utilized to analyze an elliptical airfoil.
  • The study focused on the interactions of leading-edge and trailing-edge vortices during heaving and pitching movements.
  • A history-dependent remnant vortex mechanism was examined to understand its role in the wake dynamics.
  • Bistable wake switching was observed, linked to the remnant vortex impingement mechanism.
  • Lift asymmetry was found to result from the aperiodic reversal of dipole direction due to vortex interactions.
  • A vortex-splitting process formed a metastable reverse Kármán vortex street until disturbed by ambient factors.

Abstract

Bistable wake switching is identified experimentally and numerically in an elliptical airfoil undergoing combined heaving and pitching in quiescent fluid. A history-dependent “remnant vortex impingement” mechanism drives the instability: A lingering secondary leading-edge vortex (LEV) from the preceding stroke triggers premature detachment of the nascent LEV, whose subsequent merger with the trailing-edge vortex forms an obliquely ejecting wake dipole. Aperiodic reversal of dipole direction switches the lift asymmetry despite symmetric kinematics, manifesting as nonlinear spectral sidebands in the lift spectrum. Between switching events, a vortex-splitting process facilitates a metastable symmetric reverse Kármán vortex street until disrupted by ambient disturbances.

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Cite This Study

Pinapatruni et al. (2026) studied this question.

synapsesocial.com/papers/6a0567e9a550a87e60a201e2https://doi.org/10.1063/5.0334247
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