2018
DOI: 10.1177/0954406218772603
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Singular treatment of viscous flow near the corner by using matched eigenfunctions

Abstract: In this paper, the local singular behavior of Stokes flow is solved near the salient and re-entrant corners by the matching eigenfunction method. The flow in a rectangular and an L-shaped cavity are considered as a model for the flow generated by the motion of the upper lid. The solutions of the Stokes equation in polar coordinates are matched with a velocity vector components obtained by analytic or numerical solution for the streamfunction developed for any values of the heights of the rectangular and an L-s… Show more

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Cited by 7 publications
(3 citation statements)
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“…Sprittles and Shikhmurzaev [6] considered the numerical issues arising in computations of viscous flows in corners formed by a liquid-fluid free surface and a solid boundary. In addition, Deliceoglu, et al [7] solved the local singular behavior of Stokes flow near the salient and re-entrant corners by the matching eigenfunction method.…”
Section: Introductionmentioning
confidence: 99%
“…Sprittles and Shikhmurzaev [6] considered the numerical issues arising in computations of viscous flows in corners formed by a liquid-fluid free surface and a solid boundary. In addition, Deliceoglu, et al [7] solved the local singular behavior of Stokes flow near the salient and re-entrant corners by the matching eigenfunction method.…”
Section: Introductionmentioning
confidence: 99%
“…Navier-Stokes equations regarding our system. For examples of this approach, seeGupta, Manohar, and Noble [1981] andDeliceoglu, C ¸elik, and Gürcan [2019].…”
mentioning
confidence: 99%
“…For example, the stream function of the corner flow was modelled by mirrored-driven point vortices plus a stagnation flow as a quarter of the spinup model with potential flow assumption [78,80]. The stream function of a liddriven corner flow was solved numerically by the matched eigenfunction method for a Stokes flow [81]. The similar crosswise velocity distribution pattern in the boundary layer was found by Rubin [3] between an incompressible corner flow and a quarter-infinite flat flow.…”
Section: Modelling Of Continuous Phase Dynamicsmentioning
confidence: 82%