Sinha, UN and Ramaswamy, MA (1974) Priliminary results of the computation of pressure distribution on a supercritical aerofoil. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
The preliminary results of the computation of the pressure distribution with shocks on a supercritical aerofoil using the Gerabedian and Korn's program modified to suit the IBM 370/155 Computer at Indian Institute of Technology, Madras have been reported showing the effect of the number of iterations. on the13; result and the comparison of the present results with that obtained by Garabedian and Korn.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Aerofoil |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Aerodynamics, Aerodynamics |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 30 Aug 2006 |
| Last Modified: | 24 May 2010 09:49 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2584 |
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