Kumar, Anand (1989) Flow calculation over a delta-wing using the thin-layer wavier-stokes equations. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
A 3D laminar thin-layer Navier-Stokes solver is developed13; which employs finite volume spatial discretisation and13; Runge-Kutta time integration. The code is applied to compute vortex flow over a round leading edge delta wing, and the results are compared with experiment and an Euler simulation.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Navier-stokes equatins;Vortex flow |
| Subjects: | ENGINEERING > Fluid Mechanics and Thermodynamics |
| Division/Department: | Computational and Theoretical Fluid Dynamics Division |
| Depositing User: | Mr. Ravikumar R |
| Date Deposited: | 31 Jul 2006 |
| Last Modified: | 24 May 2010 09:44 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1950 |
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