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Navier-Stokes analysis of the flow about a flap edge
- Source :
- Journal of Aircraft. Nov-Dec, 1998, Vol. 35 Issue 6, p833, 6 p.
- Publication Year :
- 1998
-
Abstract
- A study was conducted to analyze the flow associated with a flap edge, one of the three-dimensional properties of flow over a high-lift system. Structured, overset grids were utilized with an incompressible Navier-Stokes to calculate the flow over a two-element high-lift. The full-span and half-span Fowler flap configurations were then determined. Results indicated a number of flow features that significantly influence the performance of high-lift system. These include the flap-edge vortex, flow separation and spanwise lift distribution.
Details
- ISSN :
- 00218669
- Volume :
- 35
- Issue :
- 6
- Database :
- Gale General OneFile
- Journal :
- Journal of Aircraft
- Publication Type :
- Academic Journal
- Accession number :
- edsgcl.53591821