Kumar, Anand (1987) Preliminary viscous flow calculation past a wing using navier-stokes equations. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
A finite volume., multistage time-stepping, Navier-Stokes solver is being developed. Preliminary results for a low aspect ratio wing at. a subsonic Mach number and high incidence are obtained.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Viscous flow;Navier-stokes equations;Delta wing |
| Subjects: | ENGINEERING > Fluid Mechanics and Thermodynamics |
| Division/Department: | Fluid Dynamics |
| Depositing User: | Deputy Head Poornima Narayana |
| Date Deposited: | 10 Aug 2006 |
| Last Modified: | 24 May 2010 09:45 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2058 |
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