Premalatha, - and Ramamoorthy, P (1991) Performance of an airfoil at low reynolds number. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
A new airfoil performance software is developed by combining two independent codes . The first one is based on Theodorsen's thick airfoil theory and second one is a boundary layer code based on the integral method.13; The lift and pitching moment coefficients are obtained by Theodorsen's theory suitably modified for the viscous effects.The comparison between this code and NCSU code 'and experiments for a few low drag airfoil show good correlation and hence the code has great potential for further development.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Airfoil;Performance |
| Subjects: | AERONAUTICS > Aeronautics (General) |
| Division/Department: | Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division |
| Depositing User: | Mr. N A |
| Date Deposited: | 24 Jun 2006 |
| Last Modified: | 24 May 2010 09:44 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1856 |
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