4.7 Article

Conformal Mapping-Based Discrete Vortex Method for Simulating 2-D Flows around Arbitrary Cylinders

Journal

Publisher

MDPI
DOI: 10.3390/jmse9121409

Keywords

boundary method; circle theorem; conformal mapping; discrete vortex simulation; surface pressure distribution

Funding

  1. National Key Research and Development Program of China [2019YFC0312402, 2019YFC0312400]
  2. National Natural Science Foundation of China [52071056]

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A novel technique utilizing conformal mapping and the circle theorem has been developed to address the boundary penetration issue in 2D discrete vortex simulations. The technique introduces an identical vortex blob outside the body to prevent circulation loss caused by penetration into the body, maintaining constant circulation and streamlined body surfaces. Validation studies and comparisons with experimental data confirm the effectiveness of the approach.
A novel technique based on conformal mapping and the circle theorem has been developed to tackle the boundary penetration issue, in which vortex blobs leak into structures in two-dimensional discrete vortex simulations, as an alternative to the traditional method in which the blobs crossing the boundary are simply removed from the fluid field or reflected back to their mirror-image positions outside the structure. The present algorithm introduces an identical vortex blob outside the body using the mapping method to avoid circulation loss caused by the vortex blob penetrating the body. This can keep the body surface streamlined and guarantees that the total circulation will be constant at any time step. The model was validated using cases of viscous incompressible flow passing elliptic cylinders with various thickness-to-chord ratios at Reynolds numbers greater than Re = 1 x 10(5). The force and velocity fields revealed that this boundary scheme converged, and the resultant time-averaged surface pressure distributions were all in excellent agreement with wind tunnel tests. Furthermore, a flow around a symmetrical Joukowski foil at Reynolds number Re = 4.62 x 10(4), without considering the trailing cusp, was investigated, and a close agreement with the experimental data was obtained.

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