Srinivasa, K (1980) Computation of unsteady, one-dimensional flow with a shock-wave-shock fitting approach. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
This report describes the method and the computer13; program to compute the unsteady propagation of a shock13; wave in a prescribed medium like the one where density is13; varying' exponentially [1]. two-important features of . .13; the work are that (1) The shock is treated as a discontinuity arid, (2) The governing equations are cast in the nonconservative form.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Governing equations |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Aerodynamics |
| Depositing User: | Deputy Head Poornima Narayana |
| Date Deposited: | 30 Aug 2006 |
| Last Modified: | 24 May 2010 09:49 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2518 |
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