Ramamoorthy, P and Premageetha, BK (1991) 'Aerowing' - The software for aerodynamic analysis of a large aspect-ratio finite wing at low speeds. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
An existing computer software package for the determination of lift, drag and pitching moment of the finite wing is ported onto PS 386/387 system and,validated against known examples. This software is presently designated as AEROWING and is used to obtain the loads on the wing of an RPV (Remotely piloted Vehicle).quot; 13; The results prove that the software can provide a tool for the wing analysis amp; design.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Aerofoil;Pressure distribution;Finite wing |
| Subjects: | ENGINEERING > Fluid Mechanics and Thermodynamics |
| Division/Department: | Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 11 Oct 2006 |
| Last Modified: | 24 May 2010 09:51 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2942 |
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