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Dynamics of an inverted cantilever plate at moderate angle of attack

Huertas-Cerdeira, Cecilia and Goza, Andres and Sader, John E. and Colonius, Tim and Gharib, Morteza (2020) Dynamics of an inverted cantilever plate at moderate angle of attack. . (Unpublished) https://resolver.caltech.edu/CaltechAUTHORS:20200624-090733478

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Abstract

The dynamics of a cantilever plate clamped at its trailing edge and placed at a moderate angle (α ≤ 30∘) to a uniform flow are investigated experimentally and numerically, and a large experimental data set is provided. The dynamics are shown to differ significantly from the zero-angle-of-attack case, commonly called the inverted-flag configuration. Four distinct dynamical regimes arise at finite angles: a small oscillation around a small-deflection equilibrium (deformed regime), a small-amplitude flapping motion, a large-amplitude flapping motion and a small oscillation around a large-deflection equilibrium (deflected regime). The small-amplitude flapping motion appears gradually as the flow speed is increased and is consistent with a limit-cycle oscillation caused by the quasi-steady fluid forcing. The large-amplitude flapping motion is observed to appear at a constant critical flow speed that is independent of angle of attack. Its characteristics match those of the large-amplitude vortex-induced vibration present at zero angle of attack. The flow speed at which the plate enters the deflected regime decreases linearly as the angle of attack is increased, causing the flapping motion to disappear for angles of attack greater than α ≈ 28∘. Finally, the effect of aspect ratio on the plate dynamics is considered, with reduced aspect ratio plates being shown to lack sharp distinctions between regimes.


Item Type:Report or Paper (Discussion Paper)
Related URLs:
URLURL TypeDescription
http://arxiv.org/abs/2005.07374arXivDiscussion Paper
ORCID:
AuthorORCID
Goza, Andres0000-0002-9372-7713
Sader, John E.0000-0002-7096-0627
Colonius, Tim0000-0003-0326-3909
Gharib, Morteza0000-0002-2204-9302
Additional Information:C.H.-C. and M.G. acknowledge funding from the Gordon and Betty Moore Foundation. A.G. and T.C. acknowledge funding from Robert Bosch LLC through the Bosch Energy Research Network Grant (grant number 07.23.CS.15), and from the AFOSR (grant number FA9550-14-1-0328). J.S. acknowledges funding from the Australian Research Council Centre of Excellence in Exciton Science (CE170100026) and the Australian Research Council grants scheme. The authors report no conflict of interest.
Group:GALCIT
Funders:
Funding AgencyGrant Number
Gordon and Betty Moore FoundationUNSPECIFIED
Bosch Energy Research Network07.23.CS.15
Air Force Office of Scientific Research (AFOSR)FA9550-14-1-0328
Australian Research CouncilCE170100026
Record Number:CaltechAUTHORS:20200624-090733478
Persistent URL:https://resolver.caltech.edu/CaltechAUTHORS:20200624-090733478
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:103985
Collection:CaltechAUTHORS
Deposited By: Tony Diaz
Deposited On:24 Jun 2020 17:25
Last Modified:24 Jun 2020 17:25

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