Bera, Rajendra K and Ramachandra, SM (1976) Some theorems concerning drag minimization. Revue Roumaine des Sciences Techniques, Serie de Mecanique Appliquee, 21. pp. 523-529.
Full text not available from this repository.Abstract
Theorems are derived which, assuming linearized theory, show that a minimum drag wing configuration in forward flow is the same as that in reverse flow. It follows that it may be easier to design a wing in reverse flow and from this obtain the wing configuration in forward flow.
| Item Type: | Article |
|---|---|
| Uncontrolled Keywords: | Aircraft design;Drag reduction;Reversed flow;Theorems;Wing loading;Wing profiles;Aerodynamics configurations;Aerodynamic drag;Flow distribution;Left;Linearization;Optimization |
| Subjects: | AERONAUTICS > Aircraft Design, Testing & Performance |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 13 Dec 2006 |
| Last Modified: | 24 May 2010 04:24 |
| URI: | http://nal-ir.nal.res.in/id/eprint/3697 |
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