Pashilkar, AA (2001) Surface pressure model for simple delta wings at high angles of attack AIAA Paper 2001-2415. In: 19th Applied Aerodynamics Conference, 11-14 June 2001, Anaheim, CA.
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) |
PDF
2001-2415.PDF Restricted to Registered users only Download (1MB) |
Abstract
A new aerodynamic modeling approach is proposed for the longitudinal static characteristics of a simple delta wing. It captures the static variation of normal force and pitching moment characteristics throughout the angle of attack range. The pressure model is based on parametrizing the surface pressure distribution on a simple delta wing. The model is then extended to a wing/body combination where body alone data are also available. The model is shown to be simple and consistent with experimental data
| Item Type: | Conference or Workshop Item (Paper) |
|---|---|
| Additional Information: | Copyright of this article belongs to AIAA |
| Uncontrolled Keywords: | Delta Wings;Angle Of Attack;Surface Pressure;Mathematical Modelswide-body Aircraftfighter Aircraftaerodynamic Haracteristicspressure Distribution |
| Subjects: | AERONAUTICS > Aeronautics (General) |
| Depositing User: | Mr. N A |
| Date Deposited: | 20 Feb 2006 |
| Last Modified: | 27 Aug 2015 06:05 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1003 |
Actions (login required)
 |
View Item |
