Dutt, HNV (1988) Comment on 'Computation of the potential flow over airfoils with cusped or thin trailing edges'. AIAA Journal, 26 (1). pp. 122-123. ISSN 0001-1452
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Abstract
In a recent paper, Ardonceau1 developed a method for analysis13; of airfoils with cusped or thin trailing edges in inviscid13; incompressible flows using a method of singularities in a13; transformed plane. It has been stated that for thin and/or13; cusped formed trailing-edge airfoils, the surface singularity13; methods pose problems, especially near the trailing edge. This13; is demonstrated in Ref. 1 by computing pressures over a13; NACA 65012 airfoil at a 10 deg incidence where the pressure13; distribution exhibits an unrealistic loop near the trailing edge.13;
| Item Type: | Journal Article |
|---|---|
| Uncontrolled Keywords: | Aerodynamic coefficient;Computational fluid dynamics;CUSPS (Mathematics);Thin airfoils;Trailing edges;Vorticity;Boundary layers;Flat plates;Pressure distribution |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Aerodynamics |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 12 Mar 2008 |
| Last Modified: | 24 May 2010 09:55 |
| URI: | http://nal-ir.nal.res.in/id/eprint/4384 |
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