Computation of unsteady, one-dimensional flow with a shock-wave-shock fitting approach

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: Monograph (Technical Report)
Uncontrolled Keywords: Governing equations
Subjects: AERONAUTICS > Aerodynamics
Depositing User: Poornima Narayana
Date Deposited: 30 Aug 2006
Last Modified: 24 May 2010 04:19
URI: http://nal-ir.nal.res.in/id/eprint/2518

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