Accurate development of leading-edge vortex using an embedded conical grid

Kumar, Anand (1996) Accurate development of leading-edge vortex using an embedded conical grid. AIAA Journal, 1 (3). pp. 1-9. ISSN 1081-0102

Full text not available from this repository.
Official URL: http://www.aiaa.org

Abstract

The vortex formation and its development near the apex of a sharp-edged delta wing are poorly represented on conventional grids because of the dissimilar length scales of the flow and the grid. The problem is overcome by having an embedded conical grid surrounding the wing. Computed Euler solutions on such an embedded conical grid and on a conventional H-O grid are presented for a range of incidence in a subsonic freestream. The solutions on the embedded conical grid show that the vortex is well resolved right from the apex, even at a very low incidence. The vortex breakdown is well predicted on the embedded conical grid, including the case where the breakdown has just moved upstream of the trailing edge.

Item Type: Journal Article
Additional Information: Copyright for this article belongs to AIAA
Uncontrolled Keywords: Leading edges;Delta wings;Computational grids;Trailing edges; Vortex breakdown;Vortices;Angle of attack;Cartesian cordinates;Incidence;Aspect ratio
Subjects: AERONAUTICS > Aerodynamics
Division/Department: CSIR Centre for Mathematical Modelling and Computer Simulation
Depositing User: M/S ICAST NAL
Date Deposited: 05 Oct 2006
Last Modified: 24 May 2010 09:51
URI: http://nal-ir.nal.res.in/id/eprint/2856

Actions (login required)

View Item