Pashilkar, AA (2002) Surface Pressure Estimates for Pitching Aircraft Model at High Angles-of-attack13; 13;. Defence Science Journal, 52 (4). pp. 417-427.
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Abstract
The surface pressure on a pitching delta wing aircraft is estimated from the normal force and the pitching moment characteristics. The pressure model is based on parametrising the surface pressure distribution on a simple delta wing. This model is useful as a first approximation of the load distribution on the aircraft wing. Leeward surface pressure distributions computed by this method are presented.
| Item Type: | Journal Article |
|---|---|
| Uncontrolled Keywords: | Surface pressure;Delta wing aircraft;Aircraft wing;Load distribution;Aerodynamics;Vortex breakdown;Computational fluid dynamics;Surface pressure model;Angle-of-attack |
| Subjects: | AERONAUTICS > Aircraft Design, Testing & Performance |
| Division/Department: | Flight Mechanics and Control Division |
| Depositing User: | Ms. Alphones Mary |
| Date Deposited: | 22 Jun 2006 |
| Last Modified: | 24 May 2010 09:43 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1671 |
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