Physics of Fluids, Journal Year: 2025, Volume and Issue: 37(4)
Published: April 1, 2025
This study examines the aeroelastic interactions of triangular steel flags in tandem configuration for flow speed (U) up to 9.0 m/s, with inter-flag gap (Gf) ranging from 0.1 5 times leading flag's characteristic length (L). The flag is subjected both streamlined and vortex-induced flows (VIFs). Wind tunnel experiments reveal a subcritical bifurcation route limit cycle oscillations (LCOs) under flow, while VIF alters supercritical route. First, identical natural frequency 3.59 Hz (first bending mode) flutter near 7.4 m/s are tested flow. dynamics remains largely unchanged compared its standalone dynamics, trailing response highly sensitive position wake flag. Phase including locking bounded phase differences, emerges at different regimes depicting synergistic destructive coherence. For closely spaced (Gf = 0.1L), LCO amplitudes suppressed by 50%, larger gaps, increase 1.5 times. non-identical much higher (5.48 Hz) onset (U> m/s), advanced matches that oscillates close across wide range gaps speeds but exhibits small-amplitude LCOs driven very low speeds. Finally, placed downstream cylindrical bluff body examine impact conditions. Small-amplitude aperiodic observed below critical speed, which, turn, induce sufficiently strong trigger transitions periodic speeds, strongly oscillations, one locked comprehensive nonlinear analysis presented can be utilized enhancing multi-flag energy harvesting, fluid mixing, heat transfer.
Language: Английский