Computation of steady supersonic flows - two dimentional and axisymmetric13;

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: 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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