Dutta, HNV and Jacob, K (1993) Viscous subsonic flow computation for wings with flaps for high-lift. Journal of Aircraft, 30 (1). pp. 141-143. ISSN 0021-8669
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Abstract
Jacob's(1987) method is extended to the analysis of multi element wings comprising multicomponent airfoils at high lift. The approach considered includes a model for ground effect, compressibility,trailing-edge separation, and curved basic flow. First attempts to validate the method by comparing computed results with measurements are reported; within the limits of the assumptions used, the theoretical results compare well with those of experiments and the computing time requirements are modest.
| Item Type: | Journal Article |
|---|---|
| Additional Information: | Copyright for this article belongs to AIAA |
| Uncontrolled Keywords: | Mathematical models;Wings (aircraft);Computation;Lifts; Compressibility;Airfoils;Separation;Computing time;Aircraft; Computational fluid dynamics;Flaps(Control surfaces);Lift; Rectangular wings;Subsonic flow;Viscous flow;Bubbles; Iterative solution;Pressure distribution |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Experimental Aerodynamics Division, Other |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 13 Apr 2010 |
| Last Modified: | 07 Jun 2010 16:16 |
| URI: | http://nal-ir.nal.res.in/id/eprint/4427 |
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