Srinivas, K (1980) Computation of steady supersonic flows - two dimentional and axisymmetric13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
This report descrices the method and the computer program to compute steady, two-dimensional or axisymmetric,13; supersonic flows with articular reference to flow about13; blunt bodies. The method closely follows the one described13; in EutIer (1) and Kutler, Lomax and quot;Hartling (2). The13; boundary shock is treated as a discontinuity where as any13; internal Shock is allowed to be captured or in other words13; treated automatically. The computation of the interior points is carried out employiDg the second-order accurate13; MacCarmack scheme (2,3).
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Supersonic flows;Two-dimentional;Axisymmetric |
| Subjects: | AERONAUTICS > Aircraft Stability and Control MATHEMATICAL AND COMPUTER SCIENCES > Computer Systems |
| Division/Department: | Computer Support and Services Division |
| Depositing User: | Deputy Head Poornima Narayana |
| Date Deposited: | 28 Aug 2006 |
| Last Modified: | 24 May 2010 09:48 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2458 |
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