Rajeswari, B and Dutt, HNV (1988) Analysis of wing flap configurations by a nonplanar vortex lattice method. Journal of Aircraft, 25 (2). pp. 97-98. ISSN 0021-8669
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) |
PDF
4159.pdf Download (710kB) |
Abstract
A nonplanar vortex lattice method is described for calculating the potential flow aerodynamic characteristics of complex planforms, with an emphasis on wings with spanwise segmented partial-span flaps. A new technique has been developed for proper modeling of flow in the region between the flap edges and the wing in the case of part-span flaps. The effects of compressibility have been accounted for by the use of the Prandtl-Glauert rule with no approximation being made regarding freestream incidence, wing camber, and flap deflection. The method has been tested for a number of cases to assess its utility.
| Item Type: | Article |
|---|---|
| Additional Information: | Copyright for this article belongs to AIAA |
| Uncontrolled Keywords: | Aerodynamics-Wings and Airfoils;Flow of Fluids-tential Flow;Gap Modeling13; U2 - Wing Flaps13; U2 - Vortices |
| Subjects: | AERONAUTICS > Aerodynamics |
| Depositing User: | MS Jayashree S |
| Date Deposited: | 10 Mar 2010 |
| Last Modified: | 07 Jun 2010 08:02 |
| URI: | http://nal-ir.nal.res.in/id/eprint/4159 |
Actions (login required)
 |
View Item |
