Narayana, CL and Sinha, AK and Ramamoorthy, P (1976) Estimation of drag-divergence mach number for an airfoil. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
A design software package for determining the drag divergence Mach nmilber LiD is developed. The essential method is contained in the RAE data sheets. The method make s use of the Theoderson's program for incompressible flow developed by the same group. Extensive /compsrisons are made. A simple sweep correction extends the athod to sweptback wings.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Airfoil;Drag divergence |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Aerodynamics, Aerodynamics, Aerodynamics |
| Depositing User: | Deputy Head Poornima Narayana |
| Date Deposited: | 28 Aug 2006 |
| Last Modified: | 24 May 2010 09:48 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2483 |
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