Saxena, SK and Dey, Debashis (1993) High resolution TVD schemes for navier-stokes solution at13; supersonic/ hypersonic speeds. Technical Report. National Aerospace Laboratories, Bangalore, India.
Full text available as:![[img]](http://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) | PDF Restricted to Archive staff only Download (4Mb) |
Abstract
A survey of some popular upwind flux-difference schemes, both explicit and implicit, has been carried out . These schemes have reached a level of maturity where they are being increasingly used in 3D application codes for supersonic/hypersonic viscous flow computations . This is because of their ability to capture strong shocks accurately, and provide comparatively much smaller numerical dissipation within the viscous region . Different13; 3D factorisation and relaxation strategies that accompany an implicit solver are also discussed .
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Supersonic hypersonic flows;Upwind schemes;Thin-layer navier-stokea;TVD schemes;Solution |
| Subjects: | ENGINEERING > Fluid Mechanics and Thermodynamics |
| Division/Department: | Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division |
| Depositing User: | Mr. N A |
| Date Deposited: | 28 Jun 2006 |
| Last Modified: | 24 May 2010 09:42 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1589 |
Actions (login required)
| View Item |
