Evaluation of Jameson-Schmidt-Turkel dissipation scheme for hypersonic flow computations

Singh, JP (1996) Evaluation of Jameson-Schmidt-Turkel dissipation scheme for hypersonic flow computations. Journal of Aircraft, 33 (2). pp. 286-290. ISSN 0021-8669

Full text available as:
[img] PDF
Restricted to CSIR-NAL Registered users only

Download (1772Kb)
    Official URL: http://www.aiaa.org


    In the present work, the use of the Jameson-Schmidt-Turkel (JST) dissipation scheme is successfully extended to compute hypersonic flows over an airfoil. It is shown that this scheme is not only capable of computing flows at speeds all the way up to Mach 50, but also the rate of convergence and the final results are as good as those obtained using the Swanson-Turkel modification of the JST scheme and better than the Yoon-Kwak flux limited dissipation specially designed to compute high-speed flows. The scheme is seen to be so robust that it does not require a well-prepared starting solution to compute flows with either strong shocks or with high incidence, or both.

    Item Type: Journal Article
    Additional Information: Copyright for this article belongs to AIAA
    Uncontrolled Keywords: Hypersonic flow;Computational fluid dynamics;TVD schemes;Runge-kutta method;Finite volume method; Hypervelocity flow;Convergence;Navier-stokes equation; Pressure distribution;Skin friction
    Subjects: AERONAUTICS > Aeronautics (General)
    AERONAUTICS > Aerodynamics
    Division/Department: Computational and Theoretical Fluid Dynamics Division
    Depositing User: M/S ICAST NAL
    Date Deposited: 01 Mar 2010
    Last Modified: 24 May 2010 09:51
    URI: http://nal-ir.nal.res.in/id/eprint/2855

    Actions (login required)

    View Item