PreprintarXiv licencearXiv
Assessment of Numerical Lift Coefficient Data for a Circular Cylinder with Application to Bladeless Turbines
Abstract
We assess computed lift coefficient data for flow past a circular cylinder to evaluate their suitability for practical applications. Specifically, we consider lift coefficient data for a circular cylinder over Reynolds numbers from 120 to 8000. The results are obtained from two-dimensional finite element simulations of the incompressible Navier-Stokes equations using pressure robust discretizations. We compare the computed lift coefficients with published experimental and numerical results, finding good agreement in some cases but significant disagreement in others. Because lift fluctuations are central to vortex-induced vibration concepts, these data therefore provide input for the analysis and preliminary design of bladeless turbines.
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BibTeX
@misc{scott2026assessment,
title = {{Assessment of Numerical Lift Coefficient Data for a Circular Cylinder with Application to Bladeless Turbines}},
author = {L. Ridgway Scott and Henry von Wahl},
howpublished = {arXiv},
year = {2026},
month = sep,
doi = {10.48550/arxiv.2609.00850},
eprint = {2609.00850},
archivePrefix = {arXiv},
url = {https://arxiv.org/abs/2609.00850},
}
RIS
TY - UNPB
TI - Assessment of Numerical Lift Coefficient Data for a Circular Cylinder with Application to Bladeless Turbines
AU - L. Ridgway Scott
AU - Henry von Wahl
PY - 2026
DA - 2026/09/01
PB - arXiv
DO - 10.48550/arxiv.2609.00850
UR - https://arxiv.org/abs/2609.00850
AB - We assess computed lift coefficient data for flow past a circular cylinder to evaluate their suitability for practical applications. Specifically, we consider lift coefficient data for a circular cylinder over Reynolds numbers from 120 to 8000. The results are obtained from two-dimensional finite element simulations of the incompressible Navier-Stokes equations using pressure robust discretizations. We compare the computed lift coefficients with published experimental and numerical results, finding good agreement in some cases but significant disagreement in others. Because lift fluctuations are central to vortex-induced vibration concepts, these data therefore provide input for the analysis and preliminary design of bladeless turbines.
ER -