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: 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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