Ravichandran, KS and Desai, SS and Rangarajan, R (1986) Modification to the cartesian grid in 3-D potential code for flow past swept wings. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
A modification is introduced in the Cartesian grid13; construction for analysis of flow past swept wings. The13; consequent location of grid points at constant percent of local chord near the leading edge of swept wings considerably improves the computed results in this region,13; especially when the velocity distribution is peaky.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Transonic flow;Full potential equation;Wing body analysis |
| Subjects: | AERONAUTICS > Aircraft Design, Testing & Performance |
| Division/Department: | Aerodynamics, Aerodynamics, Aerodynamics |
| Depositing User: | Deputy Head Poornima Narayana |
| Date Deposited: | 01 Aug 2006 |
| Last Modified: | 24 May 2010 09:46 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2276 |
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