Rajana, BN and Viswanathan, S (1995) Comparison of two candidate airfoils for LTA application. Technical Report. National Aerospace Laboratories, Bangalore, India.
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Abstract
This report pertains to a comparative study of the performance of GAW-2 airfoil against the one designed by TSAGI for application to civil aircraft. Performance of teh two airfoils are evaluated in terms of lift coefficient, pitching moment, drag and chordwise pressure distribution. All these quantities are computed using extensively validated NGSU and DLR codes.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | airfoil; pressure distribution; drag; lift; pitching moment |
| Subjects: | ENGINEERING > Fluid Mechanics and Thermodynamics |
| Division/Department: | Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division |
| Depositing User: | Smt Bhagya Rekha KA |
| Date Deposited: | 28 Jan 2006 |
| Last Modified: | 24 May 2010 09:39 |
| URI: | http://nal-ir.nal.res.in/id/eprint/932 |
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