Abstract
This paper presents new insights on the galloping instability phenomenon of square-section prisms. The role of the orientation of the structural axes on the galloping response is studied through wind tunnel tests and quasi-steady theory. A new series of dynamic wind tunnel tests on a square section model were conducted to evaluate non-across-wind galloping vibrations, as well as conventional across-wind galloping. The results are then compared with theoretical predictions to evaluate the reliability of quasi-steady theory in assessing the galloping phenomenon. It is found that for a given angle of attack, the structure has different aeroelastic behaviour for different orientations of the principal axis. At an angle of attack close to the critical angle of attack of square prisms, the quasi-steady theory well predicts the critical wind velocity for the onset of non-across-wind galloping but it is not successful for the case of across-wind galloping.
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Acknowledgements
This research is funded by Vietnam National Foundation for Science and Technology Development (NAFOSTED) under Grant Number 107.04-2017.321. The authors would like to thank BMT Fluid Mechanics Ltd. for the use of their wind tunnel and their support and assistance during the testing campaign. Finally, the authors gratefully acknowledge the Royal Academy of Engineering Newton Research Collaboration Programme, Grant Number NRCP/1415/292, for supporting the visit of the first author to the University of Bristol.
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Nguyen, C.H., Macdonald, J.H.G. & Cammelli, S. Non-across-wind galloping of a square-section cylinder. Meccanica 55, 1333–1345 (2020). https://doi.org/10.1007/s11012-020-01166-6
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DOI: https://doi.org/10.1007/s11012-020-01166-6