Subvortex technique for the close approach to a discretized vortex sheet
The close-approach problem associated with flow calculation methods based on vortex-lattice theory is examined numerically using two-dimensional discretized vortex sheets. The analysis first yields a near-field radius of approximately the distance apart of the vortices in the lattice; only within th...
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Veröffentlicht in: | Journal of aircraft 1977-02, Vol.14 (2), p.188-193 |
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Format: | Artikel |
Sprache: | eng |
Online-Zugang: | Volltext |
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Zusammenfassung: | The close-approach problem associated with flow calculation methods based on vortex-lattice theory is examined numerically using two-dimensional discretized vortex sheets. The analysis first yields a near-field radius of approximately the distance apart of the vortices in the lattice; only within this distance from the sheet are the errors arising from the discretization significant. Various modifications to the discrete vortices are then considered with the objective of reducing the errors. This study leads to a near-field model in which a vortex splits into an increasing number of subvortices as it is approached. The subvortices, whose strengths vary linearly from the vortex position, are evenly distributed along an interpolated curve passing through the basic vortices. This subvortex technique can be extended to the three-dimensional case and is efficient because the number of vortices is effectively increased, but only where and when needed. |
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ISSN: | 0021-8669 1533-3868 |
DOI: | 10.2514/3.44582 |