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: Monograph (Technical Report)
Uncontrolled Keywords: Supersonic flows;Two-dimentional;Axisymmetric
Subjects: AERONAUTICS > Aircraft Stability and Control
MATHEMATICAL AND COMPUTER SCIENCES > Computer Systems
Depositing User: Users 60 not found.
Date Deposited: 28 Aug 2006
Last Modified: 24 May 2010 04:18
URI: http://nal-ir.nal.res.in/id/eprint/2458

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