Ramamoorthy, P and Prasad, SK (1989) Analysis and Design of Symmetrical Airfoils. Technical Report. National Aerospace Laboratories, Bangalore, India.
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Abstract
13; A new theory is developed for the analysis and design of symmetrical airfoils . It is based on Lancz s polynomial interpolation and Goldsteins approximations to thick airfoil theory . The theory gave velocity agreeing with the exact method of Theodorsen correct to three decimals . The inverse design part gave back the known airfoils coordinates again correct to three decimals .
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Design;Airfoil;Inverse resign |
| Subjects: | ENGINEERING > Fluid Mechanics and Thermodynamics |
| Division/Department: | Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division |
| Depositing User: | Deputy Head Poornima Narayana |
| Date Deposited: | 23 Jun 2006 |
| Last Modified: | 24 May 2010 09:45 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1962 |
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