Gopalakrishnan, AR and Ramamoorthy, P (1977) Determination of pressure distribution on a finite wing by kuchemann and weber method. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
A FORTRAN IV program for determining the13; pressure distribution on a finite wing is developed13; and presented here for any user. This software13; is based on the work of Kuchemann and weber and13; valid only for the incompressible flow. Conparisons13; with experiments and a sophisticated method like Multhopp's lifting surface theory have been made This quick method can be utilised for wing design also when hooked with an optimization program.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Finite wing;Lifting surface theory |
| Subjects: | MATHEMATICAL AND COMPUTER SCIENCES > Computer Programming and Software AERONAUTICS > Aerodynamics |
| Division/Department: | Aerodynamics, Aerodynamics |
| Depositing User: | Deputy Head Poornima Narayana |
| Date Deposited: | 30 Aug 2006 |
| Last Modified: | 24 May 2010 09:48 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2506 |
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